Aircraft Report for n894at



Registration History for n894at







N-Number Make Model Serial Location Description Time
N894AT BOEING 717-200 55046 SALT LAKE CITY, UT Aircraft registered to WELLS FARGO TRUST CO NA TRUSTEE, airworthiness date 2004-11-18, expiration date 2025-04-30, serial number 55046. 2021-12-23
N894AT BOEING 717-200 55046 SALT LAKE CITY, UT Aircraft registered to WELLS FARGO TRUST CO NA TRUSTEE, airworthiness date 2004-11-18, expiration date 2022-04-30, serial number 55046. 2018-12-06
N894AT BOEING 717-200 55046 SALT LAKE CITY, UT Aircraft registered to WELLS FARGO BANK NORTHWEST NA TRUSTEE, airworthiness date 2004-11-18, expiration date 2019-04-30, serial number 55046. 2015-11-19
N894AT BOEING 717-200 55046 SALT LAKE CITY, UT Aircraft registered to WELLS FARGO BANK NORTHWEST NA TRUSTEE, airworthiness date 2004-11-18, expiration date 2019-04-30, serial number 55046. 2015-11-19
N894AT BOEING 717-200 55046 SALT LAKE CITY, UT Aircraft registered to WELLS FARGO BANK NORTHWEST NA TRUSTEE, airworthiness date 2004-11-18, expiration date 2016-04-30, serial number 55046. 2013-04-17
N894AT BOEING 717-200 55046 SALT LAKE CITY, UT Aircraft registered to WELLS FARGO BANK NORTHWEST NA TRUSTEE, airworthiness date 2004-11-18, expiration date 2013-09-30, serial number 55046. 2012-04-18

Accident History for n894at


N-Number Make Model Location Description Time
N894AT BOEING 717-200 MILWAUKEE, WI ON OCT. 04, 2012 AT APPROXIMATELY 2010 CDT, A CATERING TRUCK OWNED BY AIRTRAN AIRWAYS AND OPERATED BY AN AEROTEK AVIATION EMPLOYEE CAME INTO CONTACT WITH SOUTHWEST AIRLINES DBA AIRTRAN AIRWAYS BOEING 717-200 AIRCRAFT (N894AT) THAT WAS PARKED AT GATE C14 OF MILWAUKEE MITCHELL AIRPORT (MKE). THE IMPACT RESULTED IN STRUCTURAL DAMAGE TO THE RIGHT SIDE OF THE AIRCRAFT NEAR STATIONS 207, 218, 228, 235 AND 250. N894AT OPERATED BY SOUTHWEST AIRLINES DBA AIRTRANS AIRWAYS HAD ARRIVED AT MKE AS AIRTRAN FLIGHT 725 FROM ATLANTA AIRPORT (ATL) AND NORMAL PASSENGER DEPLANING HAD BEGUN BEFORE THE DAMAGE OCCURRED. NO PERSONS ON THE AIRCRAFT OR THE GROUND WERE INJURED AS A RESULT OF THIS EVENT. 2012-10-04

Service Difficulty Reports for n894at




























































































N-Number Make Model Serial Description Time
N894AT BOEING 717200 During APPROACH - BOTH THE L1 AND R1 LOWER EXIT SIGNS WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK ABOVE SEAT 2CD, IAW B717AMM 33 -51. OPERATIONAL CHECK WAS GOOD. 2020-12-29
N894AT BOEING 717200 During INSP/MAINT - AFT CARGO COMPARTMENT STRINGER 30, STA 986 IS CORRODED. NRC 040-0008:5331-2001/001 00193: CORROSION LEVEL 1, SPLICED NEWSECTION OF LONGERON FROM STA 965-1012 REF SRM 53-20-05-2R PROC 1. 2020-06-03
N894AT BOEING 717200 During INSP/MAINT - AFT CARGO COMPARTMENT STRINGER 30, BETWEEN STA 948- 954 IS CORRODED. NRC 040-0008:5331-2001/004 00196: CORROSION LEVEL 1, SPLICED NEW SECTION OF LONGERON FROM STA 937-965 REF SRM 53-20-05-2R PROC 1. 2020-06-03
N894AT BOEING 717200 During INSP/MAINT - RAMP REPORTS DAMAGE AT AFT LOWER EDGE OF C1 CARGO DOOR. DAMAGE IS TO EXISTING DOUBLER EDGE. REMOVED, FABRICATED, AND DRILLED UP NEW DOUBLER AND TRIMED DAMAGE IAW B717 SRM 53-20-15-2R-5 OPTION 2. INSTALLED REPAIR DOUBLER PER B717 SRM 53-20-15 FIG 202 OPT. 2. ALL RII COMPLIED WITH (QC2060). (LP #6669040) 2020-05-28
N894AT BOEING 717200 During NOT REPORTED - DISBONDED 2020-04-29
N894AT BOEING 717200 During UNKNOWN - INB SPOILER HAS DELAMINATION BOTTON SURFACE. LARGE DELMINATION AREA. 2019-09-19
N894AT BOEING 717200 During INSP/MAINT - HORIZONTAL STABILIZER BEARING AND CENTER SECTION ACCESS DOORS - MEL NUMBER ADDED FOR DISPATCH RELEASE, LOG REDEFERRAL REQUIRED. ON WALK AROUND FOUND HORIZONTAL STAB BEARING COVER MISSING. DEFERRED ITEM. WILL NEED A SUPPLEMETAL SDR ONCE REAPIR IS COMPLETE. REPORTED AS AN SDR DUE TO POSSIBILITY THE PART DEPARTED THE AIRCRAFT DURING FLIGHT. (LP5082016) 2019-07-18
N894AT BOEING 717200 During INSP/MAINT - TAIL CONE SLIDE COVER WAS FOUND NOT SECURE. REPLACED A DAMAGED LATCH ON THE SLIDE COVER IAW AMM 25-61-02 AND RIG SLIDEIAW TASK CARD 2561-9006. 2018-10-15
N894AT BOEING 717200 During INSP/MAINT - EMERGENCY LIGHT LENS DAMAGED. REPLACED THE DAMAGED LENS. 2018-10-12
N894AT BOEING 717200 During INSP/MAINT - FOUND EMERGENCY LIGHT AT ESCAPE RAMP PANEL IN POOR CONDITION. REPLACED THE BRACKETS IAW SRM 51-40-02. 2018-10-12
N894AT BOEING 717200 During INSP/MAINT - RIGHT INBD SPOILER PANEL CENTER HINGE BEARING LOOSE IN BORE. THE SPOILER PANEL WAS REPLACED. 2018-10-05
N894AT BOEING 717200 During INSP/MAINT - FOUND EMERGENCY LIGHT L2-938 BROKEN AFT COMPARTMENT. REPLACED TERMINALS NEEDS LIGHT ASSY MOUNTED. MOUNTED LIGHT ASSY CKSGOOD. 2018-07-05
N894AT BOEING 717200 During INSP/MAINT - GOUGE ON THE UPPER SURFACE OF THE AFT HORIZONTAL LEG OF CANTED FRAME STA 1145 RT SIDE APPROX RBL 4-6. NRC 001-0253:5300-2004/005 00214: 566363-14 REV 1 AND ER/A 566363-14 REV O MATCH WORK COMPLIED WITH PER ER/A 566363-14 REV O. 2018-03-06
N894AT BOEING 717200 During INSP/MAINT - GOUGE ON THE UPPER SURFACE OF THE AFT HORIZONTAL LEG OF CANTED FRAME STA 1145 LT SIDE APPROX LBL 4-7. NRC 001-0253:5300-2004/004 00213: PRI 566363-14 REV 1 AND ER/A 566363-14 REV O MATCH. WORK WAS PERFORMED PER ER/A 566363-14 REV O. 2018-03-06
N894AT BOEING 717200 During INSP/MAINT - ON SVC FOUND EMERG BATT PACK INOPERATIVE. R&R BATT CHARGER / BATT B5-235 REF AMM 33-51, WDM 33-51. CHECKS GOOD. OK FOR SVC. 2017-03-29
N894AT BOEING 717200 During INSP/MAINT - LEFT OUTER CUSP WEB HAS TWO SPOTS OF CORROSION BETWEEN BS 794 - 813. BLENDED CORRODED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55 PG 101 & 102 FIG 101. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM 53-00-55 REPAIR 4 FIG 216. 2016-11-16
N894AT BOEING 717200 During INSP/MAINT - LEFT OUTER CUSP WEB CORRODED AT BS 544. CORRISION BLENDED BEYOND ALLOWABLE LIMITS. REPAIRED THE CUSP WEB IAW SRM 53-00-55 ALLOWABLE DAMAGE 1 AND 53-00-55 REPAIR 4. 2016-11-16
N894AT BOEING 717200 During INSP/MAINT - SCUFFPLATE AFT CARGO BIN HAS CORROSION. OPENED UP AFT CARGO DOOR JAMS AND REMOVED CORRODED FRAME SECTION TO FOM. ITEMTRANSFERRED TO NR 02 FOR COMPLETION. 2016-10-27
N894AT BOEING 717200 During INSP/MAINT - RIGHT CUSP WEB BS 389-503 UPPER AND LOWER SURFACES, HAS SEVERAL AREAS OF CORROSION. INSTALLED NEW CUSP WEB IAW SRM 51-41-02, SRM 51-41-01 AND SRM 51-41-05. 2016-04-27
N894AT BOEING 717200 During INSP/MAINT - LEFT OUTER CUSP WEB HAS CORROSION AROUND SEVERAL FASTENER HEADS BETWEEN BS 813 & 832. REPAIRED THE CUSP WEB IAW SRM 53-00-55, PG 101, 102 AND 104, AND FIG 216, REPAIR 4. 2016-04-27
N894AT BOEING 717200 During INSP/MAINT - DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE VENTRAL STAIRWAY SIDEWALL WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION. 2016-04-07
N894AT BOEING 717200 During INSP/MAINT - BS 1087 ABOVE STRINGER 14R, SKIN HAS A 2 DIRECTIONAL CRACK, VERTICAL LEG .5" & HORIZONAL LEG .1250". HFEC VERIFIED IAWNDT SPM 06-10-01.001 REQUEST ENGINEERING DISPOSITION. REPAIRED CRACK AT BS 1087, 514R IAW ER/A 543584-14 ASSOCIATED ER/A 00-543584 ADDED FOR AC 9554. 2016-03-29
N894AT BOEING 717200 During INSP/MAINT - LEFT CENTER TANK UPPER REAR SPAR CORRODED AT XCW 13, 18, 52, & 59L. CORROSION ON UPPER CENTER TANK WAS REPAIRED IAW ER/A 543586-14, FASTENER HOLES DAMAGED COMMON TO CORROSION BLENDOUT AREA. WERE REPAIRED IAW PRI, REV 3, 543589-14 AND ER/A543589-14, REV ORIGINAL. ASSOCIATED ER/A 54-358914 ADDED FOR AC 9554. 2016-03-29
N894AT BOEING 717200 During INSP/MAINT - BS 1022, STRINGER 14R, SKIN HAS A TWO INCH HORIZONTAL CRACK HFEC VERIFIED IAW NDT SPM 06-10-01.001 PROCEDURE 1. INSTALLED REPAIR IAW PRI 543585-14, REVISION 2, AND ER/A 543585-14 REV. 2016-03-23
N894AT BOEING 717200 During INSP/MAINT - RT CUSP SECTION, BS 389-503, UPPER AND LOWER SURFACES, HAS SEVERAL AREAS OF CORROSION. INSTALLED RT CUSP WEB AT FS 389-503 IAW SRM 51-41-02, SRM 51-41-01 AND SRM 51-41-05. 2016-03-11
N894AT BOEING 717200 During INSP/MAINT - BS 1133, 1.5" OTBD OF STR 2L HAS .1250 INCH SKIN CRACK AT SHEAR TIE FASTENER LOCATION. HFEC VERIFIED IAW NDTSPM 06-10-01, 001 PROCEDURE, 1 REF ORNRC 0300-0005. REMOVED CRACK FROM FUSELAGE SKIN AT BS 1133, OTBD OF STR 2L AND REPAIRED IAW EA543582-14AD. 2016-03-10
N894AT BOEING 717200 During INSP/MAINT - WEB FLOOR SUPPORT FWD OF R1 DOOR AND WATER LINE PAN IS CORRODED, M ON REPAIR RACK. BLEND & CHECK LIMITS. REF ORNRC 64480-0200-0140. CORRODED BEYOND LIMITS IAW SRM 53-00-00. REPLACED FLOOR SUPPORT MATCH DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-08, PG 1 TO BE INSTALLED ON ORNRC 0052. 2016-03-08
N894AT BOEING 717200 During INSP/MAINT - BS 1153, 3" INBD OF STR 3R, SKIN HAS .2500" CRACK AT SHEAR TIE FASTENER LOCATION. HFEC VERIFIED IAW NDT SPM 06-10-01. 001 PROCEDURE 1, REF: ORNRC 64480-0300-0006. REPAIRED DAMAGE AREA AT BS 1153 3" INBD OF STR 3R IAW ER/A 543583-14. AMDSCONTINUATION FORM PAGES 1-5 FOR WORK COMPLETED. 2016-02-29
N894AT BOEING 717200 During INSP/MAINT - LOWER BEAM CRACKED ON R-1 SERVICE DOOR AT LOWER END BELOW BEAM ATTACH FITTING REPAIR, REPLACE BEAM REF ORNRC 64480-0800-0029. REMOVED AND INSTALLED NEW Z FRAME IAW SRM 51-40-02, PAR 6 AND DWG 591084. 2016-02-29
N894AT BOEING 717200 During INSP/MAINT - LEFT PYLON APRON, FRAME BS 1076 UPPER LONGERON REPAIR CRACKED AT UPPER COWLING HINGE FITTING CUTOUT. INSTALLED FABED NEW DOUBLER FROM 2024-T3- .071 QQ-A- 250/S. 2024-T3 IS A PERMITTED SUBSTITUTION FOR 2024-T42 IAW SRM 51-30-08, FIG 1, TABLE A IAW SRM 54-50-02. REPAIR STEP 6F FIG 203, PG 209-210. PERFORMED FLOURESCENT PENETRANT OF DOUBLER IAW NON DESTRUCTIVE TESTING STANDARDS MANUAL 08-00-03. NO DEFECTS NOTED REINSTALLED AFT UPPER COWL HINGE FITTING IAW SRM 51-41-05, FIG 2REINSTALLED NR 1 ENGINE UPPER COWLING IAW AMM 71-12-01-400-801. 2016-02-26
N894AT BOEING 717200 During INSP/MAINT - UPPER CABIN LT ENGINE PYLON SUPPORT BULKHEAD, BS 1022 IS CRACKED ON AFT SIDE AT LONGERON 7L. MARKED, VERIFIED WITH EDDYCURRENT. CUT OUT DAMAGE AS MARKED BS 1022 L7L IAW SRM 51-70-11, FIG 201. HFEC OF CUTOUT SHOWED NO DEFECTS IAW NOT SPM 06-10-01. 001 TAG 6782. FABRICATED REPAIR DOUBLER FROM 7075-0 .090". HEAT TREAT TO 7075.T6 COMPLIED WITH ON CUSTOMER WONR 64481-0010. REPAIR FROM 7075-T6 .080" AND SHIMS FROM 7075-T6 .090 IAW SRM 51-10-04, STEP 21 AND PRIMED IAW SRM 81-70-11, REPAIR 1, FIG 1. 2016-02-25
N894AT BOEING 717200 During INSP/MAINT - ELECTRONIC EQUIPMENT COMPARTMENT A LOWER DRAIN MAST IS CORRODED, FWD OF 218 BULKHEAD BETWEEN S27-S28R. VERIFIED DRAIN MAST DOUBLER WAS OUT OF LIMITS BY VISUAL INSPECTION. ZERO THICKNESS REMAINING. REMOVED 2 EA INTERCOSTALS TO GAIN ACCESS REMOVED DRAIN MAST AND DOUBLER. FABRICATED NEW DOUBLER REINSTALLED DRAIN MAST AND DOUBLER. REINSTALLED 2 EA INTERCOSTALSIAW AMM 30-72-02-400-801, DWG 9923686, REV D, SRM 51-41-02. 2016-02-24
N894AT BOEING 717200 During INSP/MAINT - LEFT OUTER CUSP WEB HAS CORRODED LAP JOINT AT ATTACH ANGLE, BS 635. MARKED. BLENDED CORROSION ON LT UPPER CUSP ANGLE SPLICE AT BS 635 AND FOUND TO BE OUT OF LIMITS. ORIGINAL 0.080", REMAINING 0.060". FABRICATED NEW UPPER CUSP ANGLE SPLICE AND HEAT TREATED TO T6 CONDITION. ALODINED, PRIMIED, PAINTED, AND INSTALLED UPPER CUSP ANGLE SPLICE AT STA 635 IAW SRM 53-00-00, FIG 103, SPM 04-00-06, SRM 51-41-05, PAR 4, SRM 51-22-01, PAR 6A, 4, 6F, 6H AND DWG 9910151, REV CH. 2016-02-24
N894AT BOEING 717200 During INSP/MAINT - LEFT OUTER CUSP WEB HAS CORRODED LAP JOINT AT ATTACH ANGLE AT BS 589. MARKED. BLENDED CORROSION ON LEFT UPPER CUSP ANGLE SPLICE AT BS 589 AND FOUND TO BE OUT OF LIMITS. ORIGINAL 0.080", REMAINING 0.055". REMOVED UPPER CUSP ANGLE SPLICE AND FABRICATED NEW CUSP ANGLE SPLICE AND HEAT TREATED TO CONDITION T6. ALODINED, PRIMED, PAINTED, AND INSTALLED NEW CUSP ANGLE SPLICE AT BS 589 IAW SRM 51-41-05, 53-00-00, FIG 103, MD SPM 04-00-06, SRM 51-22-01 PAR 6A(4), 6F, 6H, AND DWG 9910151, REV CH. 2016-02-24
N894AT BOEING 717200 During INSP/MAINT - LH OUTER CUSP WEB HAS CORROSION AROUND SEVERAL FASTENER HEADS BETWEEN BS 813 & 832. REPAIRED LT OUTER CUSP WEB AT BS 813 TO 832 IAW SRM 53-00-55, PG 101, 102 AND 104, AND FIG 216, REPAIR 4. 2016-02-24
N894AT BOEING 717200 During INSP/MAINT - BOTH LOWER ATTACH ANGLES FOR PANEL 370AL, LT AND RT SIDES ARE CRACKED. REPLACED CRACKED ATTACH ANGLES 2 IAW SRM 51-41-02, SECTION 4, SRM 51-41-05, SECTION 8 AND ERA 510501-14MA. 2016-02-23
N894AT BOEING 717200 During INSP/MAINT - R1 DOOR AFT SUBFLOOR IS CRACKED AND HAS CORROSION. REPLACE SUBFLOOR IAW OR NRC 64480-0200-0145. FABRICATED NEW SUB FLOOR IAW DWG 9936535. APPLIED ALODINE IAW AMM 51-10-00-370-803. PRIMED AS REQUIRED IAW AMM 51-10-00-370-803. APPLIED TOPCOAT IAW AMM 51-10-00-370-803. 2016-02-23
N894AT BOEING 717200 During INSP/MAINT - DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD. 2016-01-12
N894AT BOEING 717200 During INSP/MAINT - SECOND FRAME AFT UNDER INTERIOR SCUFF PLATE AFT CARGO BIN HAS CORROSION. OPENED UP AFT CARGO DOOR JAMB AND REMOVED CORRODED FRAME SECT TO FORM. REPLACED FRAME IAW DWG 995822T. 2016-01-06
N894AT BOEING 717200 During INSP/MAINT - STRINGER 30L CORRODED AT BS 954. FABRICATED REPAIR AND INSTALLED IAW SRM 53-20-05, REPAIR 1. STRINGER INSTALLATION OK IAW SRM 53-20-05. 2016-01-06
N894AT BOEING 717200 During INSP/MAINT - AFT CARGO DOOR CUTOUT CORRODED. C/W PRI 542549-14, REV 0, REV 1, REV 2. FINAL ERA 542549-14 REV ORIGINAL C/W AND MATCHES. 2016-01-06
N894AT BOEING 717200 During INSP/MAINT - DURING SCHEDULED CHECK OF THE TAILCONE DEPLOYMENT, IT WAS NOTED THAT THE FORCE REQUIRED TO PULL THE INTERNAL RELEASE HANDLE EXCEEDED TEST LIMITS. COMPLIED WITH REPAIR ON NON-ROUTINE WC OF WO 9554 07/31/15. 2015-08-07
N894AT BOEING 717200 During INSP/MAINT - DURING SPECIAL VISIT FOR OVERWING FRAME INSPECTION, IT WAS NECESSARY TO CUT AND SPLICE STR 11 RT STA 655-674 FOR REMOVALOF FRAME 674 RT. INSTALLED REPAIR SPLICE IAW ER/A 530437-14MA. 2015-03-11
N894AT BOEING 717200 During INSP/MAINT - REMOVED CUSP WEB FROM STA 655 TO STA 715 RT SIDE. REPLACED CUSP WEB IAW SRM 51-41. WEB WAS REMOVED TO PERFORM OVERWINGFRAME REPLACEMENT DUE TO AD MANDATED INSPECTION FINDINGS. 2015-03-11
N894AT BOEING 717200 During INSP/MAINT - DURING FRAME INSPECTION IN MSP, FOUND CRACK INDICATION ON RT SIDE FRAME 674 WITH EDDY CURRENT. REPLACED OVERWING FRAMEAT STA 675 RT IAW AMDS WC 5310-01436-03B. 2015-03-11
N894AT BOEING 717200 During INSP/MAINT - DURING SPECIAL VISIT IN MSP, FOUND CRACK INDICATION ON RT SIDE FRAME 715 WITH EDDY CURRENT. REPLACED OVERWING FRAME ATSTA 715 RT IAW AMDS WC 5310-01436-03B. 2015-03-11
N894AT BOEING 717200 During INSP/MAINT - REMOVED OTBD RT SEAT TRACK FROM STA 589 TO STA 746 TO FACILITATE OVERWING FRAME REPLACEMENT DUE TO AD MANDATED OVERWINGFRAME INSPECTION FINDINGS. 2015-03-11
N894AT BOEING 717200 During INSP/MAINT - DURING INSPECTION, THE TEE ANGLE AT BS 715, LBL 44 WAS FOUND TO BE CRACKED. REPLACED TEE ANGLE IAW DWG 9923417. 2015-02-12
N894AT BOEING 717200 During INSP/MAINT - SEAT TRACK DAMAGED BS 737 LBL 44. REPAIRED IAW ER/A 531461-14. 2015-02-12
N894AT BOEING 717200 During INSP/MAINT - RT FLOORBEAM CRACKED AT RADIUS. BS 737, RBL 54. REPLACED CRACKED FLOORBEAM TEE RBL 19 TO RBL 60 IAW SRM 51-40-08, 51-41-05 AND DWG 5930561, REV AC. 2015-02-12
N894AT BOEING 717200 During INSP/MAINT - FLOORBEAM BS 737 LT BETWEEN LBL 54 AND LBL 50, CRACKED. REPLACED THE FLOORBEAM ANGLE LBL 19 TO LBL 60 IAW SRM 51-40-08, 51-41-05 AND DWG 5930561, REV AC. 2015-02-12
N894AT BOEING 717200 During INSP/MAINT - VERTICAL SUPPORT ANGLE AT STA 737, LBL 44 WAS FOUND TO BE CRACKED. REPLACED VERTICAL SUPPORT IAW SRM 51-40-08, DWG 5940863, REV N AND DWG 9923417, REV B. 2015-02-10
N894AT BOEING 717200 During INSP/MAINT - VERTICAL SUPPORT ANGLE AT BS 737, RBL 44 WAS FOUND TO BE CRACKED. REPLACED CRACKED VERTICLE SUPPORT PN 3925812U2 AT STA737 RBL 44 IAW SRM 51-40-08 AND DWG 5940863, REV N AND DWG 9923417, REV B. 2015-02-10
N894AT BOEING 717200 During INSP/MAINT - TAIL COMPARTMENT AFT EMERGENCY EXIT LIGHT BULB INOPERATIVE. REPAIRED BULB IAW MM. 2014-03-13
N894AT BOEING 717200 During INSP/MAINT - RT FWD OVERWING DOOR EMERGENCY LIGHT BULB INOPERATIVE. REPAIRED BULB IAW MM. 2014-03-13
N894AT BOEING 717200 During INSP/MAINT - LT WING FWD BULKHEAD CTR WING UPPER SKIN CORRODED ALONG THE EDGES. REPAIRED SKIN IAW SRM. 2014-03-10
N894AT BOEING 717200 During INSP/MAINT - RT WING FLAP INBD FIXED VANE UPPER SKIN SURFACE DELAMINATED. REPAIRED SKIN IAW SRM. 2014-03-06
N894AT BOEING 717200 During INSP/MAINT - SKIN CRACKED BETWEEN BS 514 TO BS 541, BETWEEN LONGERON 24L TO STRINGER 25L. REPAIRED SKIN IAW SRM. 2014-03-06
N894AT BOEING 717200 During INSP/MAINT - SHEAR TIE CRACKED AT BS 1144, STRINGER 2R. R & R SHEAR TIE IAW SRM. 2014-03-05
N894AT BOEING 717200 During INSP/MAINT - STRINGER CRACKED AT BS 1133, LONGERON 2L. REPAIRED STRINGER IAW SRM. 2014-03-05
N894AT BOEING 717200 During INSP/MAINT - AFT CABIN EMERGENCY EXIT LIGHT ASSEMBLY ABOVE AFT ACCESSORY COMPARTMENT DOOR MISSING. INSTALLED LIGHT IAW AMM. 2014-03-05
N894AT BOEING 717200 During INSP/MAINT - RT WING FLAP NR 4 RIB DAMAGED. REPAIRED NR 4 RIB IAW SRM & DRAWING. 2014-03-05
N894AT BOEING 717200 During INSP/MAINT - RT WING FLAP OTBD UPPER SKIN SECTION DAMAGED. REPAIRED SKIN IAW SRM & DRAWING. 2014-03-05
N894AT BOEING 717200 During INSP/MAINT - FWD CARGO DOOR JAMB PAN CORRODED. R & R PAN IAW SRM. 2014-03-05
N894AT BOEING 717200 During INSP/MAINT - FRAME CRACKED AT BS 522, BETWEEN LONGERON 24L TO LONGERON 26L. REPAIRED FRAME IAW SRM. 2014-03-05
N894AT BOEING 717200 During INSP/MAINT - FRAME CORRODED AT BS 908 BETWEEN LONGERON 27L TO LONGERON 27R. REPAIRED FRAME IAW SRM. 2014-02-25
N894AT BOEING 717200 During INSP/MAINT - FRAME CORRODED AT BS 889 BETWEEN LONGERON 27L TO LONGERON 27R. REPAIRED FRAME IAW SRM. 2014-02-25
N894AT BOEING 717200 During INSP/MAINT - FRAME CORRODED AT BS 927 BETWEEN LONGERON 27L TO LONGERON 27R. REPAIRED FRAME IAW SRM. 2014-02-25
N894AT BOEING 717200 During INSP/MAINT - AFT LT LAVATORY EMERGENCY LIGHT BROKEN. R & R LIGHT IAW AMM. 2014-02-24
N894AT BOEING 717200 During INSP/MAINT - MAIN CABIN DOUBLER CUSP WEB CRACKED AT BS 674 RBL 44. REPAIRED DOUBLER IAW SRM. 2014-02-20
N894AT BOEING 717200 During INSP/MAINT - MAIN CABIN DOUBLER CUSP WEB CRACKED AT BS 674 LBL 44. REPAIRED DOUBLER IAW SRM. 2014-02-20
N894AT BOEING 717200 During INSP/MAINT - LT WING NR 5 SLAT OTBD END FITTING CRACKED, R & R FITTING IAW SRM & DRAWING. 2014-02-18
N894AT BOEING 717200 During UNKNOWN - LOWER FWD EMERGENCY FLASHLIGHT INDICATOR NOT FLASHING. REPLACED BATTERY AND OPS CHECKED REF AMM. 2013-04-09
N894AT BOEING 717200 During UNKNOWN - TAIL CONE EMERGENCY EXIT SIGN INTERMITTENTLY ILLUMINATED WITH EMERGENCY LIGHT SWITCH IN ARM POSITION. (MOSTLY ON). REMOVED AND REPLACED AFT EMERGENCY BATTERY/POWER SUPPLY, TAIL EXIT SIGN OP CHECK GOOD. IAW AMM 33-51-03. PARTS VERFIED 77009 2013-02-08
N894AT BOEING 717200 During INSP/MAINT - FRAME CORRODED AT BS 889, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM. 2012-10-22
N894AT BOEING 717200 During INSP/MAINT - FRAME CORRODED AT BS 927, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM. 2012-10-22
N894AT BOEING 717200 During INSP/MAINT - FRAME CORRODED AT BS 908, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM. 2012-10-22
N894AT BOEING 717200 During UNKNOWN - L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD LOOSE. SECURED LANYARD PER MM. 2012-10-10
N894AT BOEING 717200 During UNKNOWN - L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LANYARD LOOSE. SECURED LANYARD PER AMM. 2012-10-10
N894AT BOEING 717200 During INSP/MAINT - L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER AMM. 2012-09-27
N894AT BOEING 717200 During INSP/MAINT - GIRT BAR WILL NOT CLIP INTO PLACE ON L1 DOOR. CLEARED DEBRIS FROM RETAINER, OPS CHECK OK, MM 52-11, 25-61. 2011-12-21
N894AT BOEING 717200 During INSP/MAINT - FWD CABIN ATTENDANT PANEL EMERGENCY LIGHT SWITCH INOP. REMOVED AND REPLACED BATTERY ASSY AT AFT CARGO COMP IAW B717 MM33-51, OPS CHECK OK. 2011-11-22
N894AT BOEING 717200 During INSP/MAINT - FWD CABIN ATTENDANT PANEL EMERGENCY LIGHT SWITCH INOP. REMOVED AND REPLACED BATTERY ASSY AT AFT CARGO COMP IAW B717 MM33-51 / OPS CHECK OK. 2011-11-17
N894AT BOEING 717200 During INSP/MAINT - AFT CARGO COMPARTMENT LONGERON SUPPORT, STA 1152, LONG L1L TO L2L, CRACKED. ACCOMPLISHED LONGERON SUPPORT REPLACEMENT PER EA 17-53-02519IR. 2010-12-10
N894AT BOEING 717200 During INSP/MAINT - RIGHT PYLON APRON LOWER NR 2 HINGE CUT OUT AREA, CRACKED. ACCOMPLISHED NR 2 HINGE CUTOUT AREA DOUBLER REPAIR PER B717 SRM 54-50-02 FIG 203 REP 1. 2010-11-23
N894AT BOEING 717200 During INSP/MAINT - RIGHT PYLON APRON UPPER NR 2 HINGE CUTOUT AREA, CRACKED. ACCOMPLISHED NR 2 HINGE CUTOUT AREA DOUBLER REPAIR PER B717 SRM 54-50-02 FIG 203 REP 1. 2010-11-23
N894AT BOEING 717200 During INSP/MAINT - LIGHT LENS COVER MISSING AT ROW 17 FOR CABIN CEILING LIGHTING. LIGHT WORKS. INSTALLED LENS COVER REF AMM 33-51. 2010-07-21
N894AT BOEING 717200 During INSP/MAINT - TAIL CONE SLIDE INADVERTENTLY DEPLOYED BY MAINTENANCE. REPLACED TAIL CONE SLIDE ASSEMBLY PER B717 MM 25-61-02. REINSTALLED TAIL CONE ASSEMBLY PER B717 MM 53-52-01. 2008-12-22
N894AT BOEING 717200 During INSP/MAINT - AFT CARGO COMPARTMENT DOOR LOWER PAN CORRODED BEYOND LIMITS. REMOVED AND REPLACED LOWER DOOR PAN SPLICE SECTION PER SRM53-20-15. 2008-12-22
N894AT BOEING 717200 During CRUISE - AT CRUISE ALTITUDE CABIN INFLOW LOW MESSAGE CAME ON QRH PROCEDURES FOLLOWED AND DESCENT TO FL 24.0 WA BEGUN. CABIN CONTINUED TO CLIMB W/OUT FLOW, VALVE CLOSED DURING DESCENT. CABIN ALT REACHED 12,000 AT MAXIMUM. DESCENT CONTINUED UNTIL CABIN BELOW 10,000'. LATER DURING FLIGHT CABIN INFLOW LOW MESSAGE WENT AWAY, MANUAL PRESSURE WAS USED AT A/C ALT AT 11,000. REMOVED AND REPLACED NR 2 CPC. 2005-02-18
N894AT BOEING 717200 During CRUISE - CABIN INFLOW LOW, CABIN CLIMBED 300-400 FT/MIN BEST CASE 1700-1800 FT/MIN WORST CASE, FORCED DESCENT TO MAINTAIN CABIN ALTITUDE OUTFLOW. VALVE FAILED TO CLOSE IN AUTO OR MANUAL. REMOVED AND REPLACED CPC. 2005-01-31

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Aviation Datasets Explained


Aircraft Lookup allows anyone to quickly search public datasets published by various aviation administrative services as well as marketplaces and other private aviation data providers in the United States. These datasets provide valuable insight into the history and maintenance record of any aircraft registered in the US. When you provide an N-Number above, we cross reference historical SDR, FAA, and NTSB datasets to identify any relevant records related to that N-Number.

As you may be aware, N-Numbers are not connected to an aircraft for the life of that aircraft - N-Numbers may be deregistered, and re-registered to completely different aircraft. For that reason, please confirm that the details of any search result correspond to the make and model you intended to pull records for.

SDR, FAA, and NTSB databases are provided as follows:

The Service Difficulty Reports (SDR) dataset is defined as "[t]he reports submitted by certificate holders and certificated repair stations, known as service difficulty reports (SDR's), provide the FAA with airworthiness statistical data necessary for planning, directing, controlling, and evaluating certain assigned safety-related programs." This data is, in its raw form, a tab-delimited file with encoded field headers.

The FAA Registration dataset is fairly straightforward - it is a listing of current registrations (along with addresses, aircraft serial number, and other basic metadata) at any point in time. The registration data is a comma delimited file that has named fields at the top of each file. The FAA provides historical data on their site for the previous few years.

The FAA Accident/Incident dataset covers a range of accidents and incidents that may or may not overlap with NTSB data. Typically, more significant crashes are covered by NTSB data while less significant crashes are more comprehensively covered by the FAA Accident/Incident data, which will frequently include minor events like gear-up landings and so forth. The data provided by the FAA is in a tab-delimited file with encoded field headers.

The NTSB investigation dataset is distinct from the FAA dataset. While the number of accidents or incidents they cover are less numerous, the depth at which they are covered is significantly deeper when reported by the NTSB. While each record from the NTSB contains incredible amounts of metadata related to people responsible for the flight, prevailing meteorological conditions at the time of flight, and passengers aboard, this aircraft lookup tool only provides basic summary data. The full dataset is provided as a series of Microsoft access file databases on the NTSB site.