# Service difficulty reports: N891AT

A list on [N891AT](https://openairdocs.org/aircraft/N891AT.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 140 reports

- [SDR DALA2026101305629](https://openairdocs.org/sdr/DALA2026101305629.md): Spar · cracked · Oct 10, 2026 · N891AT · Boeing 717200 · Wing Spar
  > CRACK INDICATION ON LH WING REAR SPAR INBD. STA 150.45 XRS-177 BEHIND "T" ANGLE. REPAIRED PER ERA 636800-14AD. (1858405) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026101305624](https://openairdocs.org/sdr/DALA2026101305624.md): Spar · cracked · Oct 10, 2026 · N891AT · Boeing 717200 · Wing Spar
  > CRACK INDICATION ON LH WING REAR SPAR INBD STA XRS=150.45-177 BEHIND T ANGLE. REPAIRED PER ERA 636800-14AD. (8818554) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026101205598](https://openairdocs.org/sdr/DALA2026101205598.md): Spar Cap · cracked · Oct 9, 2026 · N891AT · Boeing 717200 · Wing Spar
  > LEFT WING REAR SPAR LOWER CAP AFT FLANGE CRACKED. REPAIRED PER ER/A 636800-14AD. (1857017) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026100205475](https://openairdocs.org/sdr/DALA2026100205475.md): Doubler · cracked · Oct 1, 2026 · N891AT · Boeing 717200 · Wing, Landing Gear Attach Fittings
  > FOUND TWO CRACK INDICATION IN THE LT UPPER MLG DOUBLER, COMPLIED WITH ER/A 637001-14. (1842759) (AIRCRAFT GROUNDED).
- [SDR DALA2026093005425](https://openairdocs.org/sdr/DALA2026093005425.md): Spar · cracked · Sep 29, 2026 · N891AT · Boeing 717200 · Wing Spar
  > LT WING CENTER BUTE DOOR AFT SPAR FLANGE, CRACK INDICATION IN THE 13TH HOLE OTBD OF THE SPAR SPLICE, INSTALLED OVER SIZE HILOK REF B717 SRM 51-41-05. (1839494) (AIRCRAFT GROUNDED).
- [SDR DALA2026092905410](https://openairdocs.org/sdr/DALA2026092905410.md): Fitting · corroded · Sep 26, 2026 · N891AT · Boeing 717200 · Trailing Edge Flaps
  > LEFT WING INBOARD FLAP FWD FITTING CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 00-637122. (1833480) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026090404998](https://openairdocs.org/sdr/DALA2026090404998.md): Doubler · demodification · Sep 3, 2026 · N891AT · Boeing 717200 · Standard Practices/Structures
  > FOUND EXISTING (DEMOD) ANTENNA, INCLUDING AN INTERNAL DOUBLER, INTERFERING WITH STC DOUBLER BETWEEN Y503 TO Y522 AND STRG L-1 TO STRG L-3R, COMPLIED WITH ER/A 636674-14. (1793216) (AIRCRAFT GROUNDED).
- [SDR DALA2026090404997](https://openairdocs.org/sdr/DALA2026090404997.md): Doubler · misrepaired · Sep 3, 2026 · N891AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FOUND PCS DOUBLER LOCATED IN INCORRECT FRAME STATIONS, COMPLIED WITH ER/A 636674-14AD. (1793776) (AIRCRAFT GROUNDED).
- [SDR DALA2026081904727](https://openairdocs.org/sdr/DALA2026081904727.md): Panel · cracked · Aug 19, 2026 · N891AT · Boeing 717200 · Wing Main, Frame Structure
  > SHIP 9551 FOUND PANEL 530MB (ON LEFT WING BUTE DOOR) SCREW HOLE CRACKED TO EDGE OF PANEL AND STARTING INBOARD, CORRECTIVE ACTION: COMPLIED WITH ER/A 14-636156. (8818532) (AIRCRAFT GROUNDED).
- [SDR DALA2026080604542](https://openairdocs.org/sdr/DALA2026080604542.md): Panel · cracked · Aug 5, 2026 · N891AT · Boeing 717200 · Fuselage Main, Structure
  > FOUND PANEL 530MB ON LEFT WING BUTTE DOOR SCREW HOLE CRACKED, COMPLIED WITH ER/A 636156-14. (9087770) (AIRCRAFT GROUNDED).
- [SDR DALA2026052803225](https://openairdocs.org/sdr/DALA2026052803225.md): Not Reported · cracked · May 22, 2026 · N891AT · Boeing 717200 · Fuselage Structure (General)
  > REF STEP #8 RC AA5530-01048-02 AND AD 2018-10-08 4 CRACK INDICATIONS BELOW ZFS = 52.267. REPAIRED ON ERA 564482-14AD (8342877) (AIRCRAFT GROUNDED)
- [SDR DALA2026010500068](https://openairdocs.org/sdr/DALA2026010500068.md): Unknown · odor · Jan 1, 2026 · N891AT · Boeing 717200 · Air Distribution System
  > ATB, PERFORMED AN AIR TURN BACK DUE TO A FUME OR ODOR CONSISTENT WITH A WET DIRTY SOCK SMELL. MAINTENANCE COMPLIED WITH ALL NO-GO MSI STEPS AND REPLACED THE LEFT ENGINE BUFFERED AIR VALVE FOR PRECAUTIONARY.(8152312)
- [SDR DALA2025111808421](https://openairdocs.org/sdr/DALA2025111808421.md): Battery Pack · no test · Nov 15, 2025 · N891AT · Boeing 717200 · Emergency Lighting
  > DURING SERVICE CHECK, FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT LOCATION B5-259 IAW AMM 33-51. ALL LIGHTS WORK NORMAL. OK FOR SVC. (8218009).
- [SDR DALA2025071205248](https://openairdocs.org/sdr/DALA2025071205248.md): Slide · no test · Jul 11, 2025 · N891AT · Boeing 717200 · Escape Slide
  > AIRCRAFT 9551, SLIDE FAILED DEPLOYMENT TEST PER AMDS WORK CARD 2561-9003 FORCAST# 95-0525-8-0131. CORRECTIVE ACTION: SLIDE FAILED TO DEPLOY DUE TO A BROKEN CABLE P/N 2919845. REPLACED KEVLAR TAIL CONE CABLE REF B717 AMDS WORKCARD 2561-9003. (LP 7297639)
- [SDR DALA2025032102131](https://openairdocs.org/sdr/DALA2025032102131.md): Lamp · inoperative · Mar 20, 2025 · N891AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHTS FOR THE RH AFT EMERGENCY EXIT AND THE LH AFT LAVATORY WERE FOUND INOPERATIVE. SUMMARY OF NRC 00168: THE LAMPS FOR THE EMERGENCY LIGHTS AT THE RH AFT EMERGENCY EXIT AND LH AFT LAVATORY WERE REPLACED PER B717 AMM 33-52-18. THE SYSTEM NOW OPE
- [SDR DALA2025031702027](https://openairdocs.org/sdr/DALA2025031702027.md): Vane · cracked · Mar 15, 2025 · N891AT · Boeing 717200 · Leading Edge Devices
  > CRACK ON UPPER SURFACE OF FLAP MOVABLE VANE AT LH WING. SUMMARY OF NRC 00063: FLAP MOVABLE VANE AT LH WING WAS REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL IN REFERENCE WITH B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #0859916)
- [SDR DALA2025031702023](https://openairdocs.org/sdr/DALA2025031702023.md): Intercostal · cracked · Mar 14, 2025 · N891AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL STA Y=636 APPROX BL=0 AT FOWARD CARGO COMPARMENT WAS FOUND. SUMMARY OF NRC 00146: INTERCOSTAL ON STA Y=636 APPROX BL=0 AT FOWARD CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1. (LP #0858310)
- [SDR DALA2024060305739](https://openairdocs.org/sdr/DALA2024060305739.md): Battery Pack · inoperative · Jun 2, 2024 · N891AT · Boeing 717200 · Emergency Lighting
  > ON SERVICE CHECK, MAINTENANCE FOUND THAT BOTH OF THE FWD OVERWING UPPER EMERGENCY EXIT LIGHTS WERE INOPERATIVE. THE #6 &#7 EMERGENCY LIGHT BATTERY PACKS WERE REPLACED REF B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD. (LP #5891524)
- [SDR DALA2024052005347](https://openairdocs.org/sdr/DALA2024052005347.md): Battery · failed · May 18, 2024 · N891AT · Boeing 717200 · Emergency Lighting
  > THE FWD L1 DOOR EMERGENCY LIGHT IS INOPERATIVE. CONDITION WAS FOUND ON SERVICE CHECK. MAINTENANCE FOUND THE BATTERY ASSEMBLY BAD AND REPLACED IT IN REF TO B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5308068)
- [SDR DALA2023082406886](https://openairdocs.org/sdr/DALA2023082406886.md): Unknown · unknown · Aug 21, 2023 · N891AT · Boeing 717200 · Landing Gear System
  > SHIP 9551 -ATB- THE CREW NOTED STRONG AIRFRAME VIBRATION AS THE AIRCRAFT ACCELERATED THROUGH 300 KTS AT 15,000 FT. THE VIBRATION WAS FELT THROUGH THE YOKE, SEATS, AND COULD EVEN BE HEARD. THE VIBRATION STOPPED AS THE AIRCRAFT SLOWED BELOW 285 KTS. AN EMERGENCY
- [SDR DALA2023071205669](https://openairdocs.org/sdr/DALA2023071205669.md): Unknown · unknown · Jul 7, 2023 · N891AT · Boeing 717200 · Emergency Lighting
  > THE AFT EXIT DOOR EMERGENCY LIGHT ILLUMINATED WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AND POWER SUPPLY (B5-260) IAW B717 FRM FIM 33-50-00 810-801. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #4397
- [SDR DALA2023071205668](https://openairdocs.org/sdr/DALA2023071205668.md): Unknown · unknown · Jul 7, 2023 · N891AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY LIGHT IS FLICKERING ON THE L SIDE OF GRATE. IS NOT RELATED TO AIR SWITCH/CONTROLS. *** CONTRACT MAINTENANCE EVENT - OCM: 265651 *** RESET EMERGENCY LIGHT C/B. THE AFT EMERGENCY LIGHTS NOW OPERATES NORMALLY REF B717 AMM 33-51. (LP #2854005)
- [SDR DALA2023042503240](https://openairdocs.org/sdr/DALA2023042503240.md): Unknown · unknown · Apr 23, 2023 · N891AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON PAN (FASTENER HOLE AREA) ABOVE SEAL RETEINER AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00214: PAN ON FWD CARGO DOOR COMPARTMENT WAS REPAIRED PER ER/A 607572-14 REV ORIGINAL SECTION A, B, AND C AND PRI 607572-14 REV 1, SECTION A, B, AND C. ASSOCIAT
- [SDR DALA2023042503236](https://openairdocs.org/sdr/DALA2023042503236.md): Unknown · unknown · Apr 21, 2023 · N891AT · Boeing 717200 · Fuselage Structure (General)
  > CRACK ON INTERCOSTAL STA Y1110 AND STRINGERS R24 AND R25 AFT ACCESSORIES. SUMMARY OF NRC 00318: STRINGERS R25 STA Y=1110 WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 2 REPAIR 2. (LP #2730639)
- [SDR DALA2023042103141](https://openairdocs.org/sdr/DALA2023042103141.md): Unknown · unknown · Apr 20, 2023 · N891AT · Boeing 717200 · Entrance Stairs
  > DURING STEP 3 AMDS 2060-1001 CORROSION WAS FOUND ON FWD PASSENGER STAIRWELL DOOR (CPAX). SUMMARY OF NRC 540: CORROSION LEVEL 2. FORWARD STAIRWELL DOOR WAS REPLACED PER B-717 AMM 52-63-01-020-801 AND AMM 52-63-01-420 -801. (LP #2729492)
- [SDR DALA2023042103139](https://openairdocs.org/sdr/DALA2023042103139.md): Unknown · unknown · Apr 20, 2023 · N891AT · Boeing 717200 · Fuselage Structure (General)
  > FOUND CORROSION ON FITTING FOR FIXED STRUT AT AFT FACE RH MLG. SUMMARY OF NRC 00489: CORROSION LEVEL 2. FITTING FOR FIXED STRUT AT AFT FACE RH MLG WAS REPAIRED PER PRI 607264-14 REV 0 AND ER/A 607264-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #2729276)
- [SDR DALA2025013000726](https://openairdocs.org/sdr/DALA2025013000726.md): None · none · Apr 19, 2023 · N891AT · Boeing 717200 · Standard Practices/Structures
  > DTA MONITOR INSPECTION LOG REF ERA 606978-14 PENDING DTE APPROVAL DUE PRIOR TO 11APR25. DISCONTINUE REVENUE SERVICE ON OR BEFORE 11APR25 PENDING DTE APPROVAL FROM ENABLING TECHNOLOGIES. ASSOCIATED ER/A 95-606978 ADDED FOR AC 9551. UPDATED MONITOR TITLE. **REDE
- [SDR DALA2023042003109](https://openairdocs.org/sdr/DALA2023042003109.md): Unknown · unknown · Apr 19, 2023 · N891AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON FUSELAGE SKIN Y=1037 BTW L13-RH & L14-RH. SUMMARY OF NRC 00043: FUSELAGE SKIN Y=1037 BTW L13-RH & L14-RH WAS REPAIRED PER PRI 606978-14 REV.2 AND ER/A 606978-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-606978 ADDED FOR AC 9551. (L
- [SDR DALA2023041803046](https://openairdocs.org/sdr/DALA2023041803046.md): Unknown · unknown · Apr 14, 2023 · N891AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKS ON FRAMES STA Y=1022 AND STR 7L/7R AT C PAX (BOTH SIDE). SUMMARY OF NRC 00373: FRAMES STA Y=1022 AND STR 7L/7R AT C PAX (BOTH SIDE) WERE REPAIRED PER PRI 607334-14 REV 0 AND ER/A 607334-14 REV O SECTION I. PERMANENT REPAIR. (LP #2719829)
- [SDR DALA2023041402965](https://openairdocs.org/sdr/DALA2023041402965.md): Unknown · unknown · Apr 14, 2023 · N891AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORTS (2EA) BTW STA 148-200, X=7 AND X=-7 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. (W1). SUMMARY OF NRC 00356: CORROSION LEVEL 2. FLOOR SUPPORTS (2EA) BTW STA 148-200, X=7 AND X=-7 AT FLIGHT COMPARTMENT FLOOR STRUCTURE WERE REPLACED PER DW
- [SDR DALA2023041402964](https://openairdocs.org/sdr/DALA2023041402964.md): Unknown · unknown · Apr 14, 2023 · N891AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT BTW STA 157-200 FROM X=44. SUMMARY OF NRC 00523: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 157-200 FROM X=44 WAS REPLACED PER B717-200 SRM 51-40-08-0G PAR 3, SRM 51-10-04-0G. PAR 26(C) AND SRM 51-41-05-0G. (LP #2718715)
- [SDR DALA2023041402963](https://openairdocs.org/sdr/DALA2023041402963.md): Unknown · unknown · Apr 13, 2023 · N891AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STA Y=179 BTW X=-8 TO X=-40, ALSO ON FLOOR SUPPORT BTW STA Y=157-195 AND X=-44 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. (W1). SUMMARY OF NRC 00357: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=179 BTW X=-8 TO X=-40, ALSO ON FLOOR SUPPORT BTW
- [SDR DALA2023041402962](https://openairdocs.org/sdr/DALA2023041402962.md): Unknown · unknown · Apr 13, 2023 · N891AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STA Y=194 BTW X=15 AND X=44. SUMMARY OF NRC 00524: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=194 BTW X=15 AND X=44 WAS REPLACED PER B717-200 SRM 51-41-05-0G AND SRM 51-41-02-0G. (LP #2718337)
- [SDR DALA2023041302909](https://openairdocs.org/sdr/DALA2023041302909.md): Unknown · unknown · Apr 13, 2023 · N891AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STA Y=200 BTW X=- 8 AND X=-44 AT PAX COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00362: CORROSION LEVEL 2. FLOOR SUPPORT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2717156)
- [SDR DALA2023041302908](https://openairdocs.org/sdr/DALA2023041302908.md): Unknown · unknown · Apr 13, 2023 · N891AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT STA 200 AND X=-46 AT FLIGHT COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00435: CORROSION LEVEL 2. FLOOR SUPPORT STA 200 AND X=-46 AT FLIGHT COMPARTMENT FLOOR STRUCTURE WAS REPLACE PER B717-200 SRM 51-41-05-0G AND SRM 51-41-02-0G
- [SDR DALA2023041302907](https://openairdocs.org/sdr/DALA2023041302907.md): Unknown · unknown · Apr 12, 2023 · N891AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND BTW L13-RH TO L14-RH. SUMMARY OF NRC 00041: EXTERNAL FUSELAGE SKIN STA Y=1076 AND BTW L13-RH TO L14-RH WAS REPAIRED PER PRI 607016-14 REV 1 AND ER/A 607016-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #271666
- [SDR DALA2023041302906](https://openairdocs.org/sdr/DALA2023041302906.md): Unknown · unknown · Apr 12, 2023 · N891AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > IN REF 429: CORROSION OUT LIMITS ON RH CENTER SEAT TRACK BTW STA 899-970 AT PAX COMPARTMENT. SUMMARY OF NRC 00516: SEAT TRACK BTW STA 899-970 AT PAX COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-01-0G. (LP #2716662)
- [SDR DALA2023041302905](https://openairdocs.org/sdr/DALA2023041302905.md): Unknown · unknown · Apr 12, 2023 · N891AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1087 AND BTW L13-RH TO L14-RH. SUMMARY OF NRC 00042: EXTERNAL FUSELAGE SKIN STA Y=1087 AND BTW L13-RH TO L14-RH WAS REPAIRED PER PRI 607016-14 REV 1 AND ER/A 607016-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (LP #271652
- [SDR DALA2023041202863](https://openairdocs.org/sdr/DALA2023041202863.md): Unknown · unknown · Apr 12, 2023 · N891AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON CUSP WEB (INNER AND UPPER SURFACE) BTW STA 503-522, BTW STA 541-560, ALSO BTW STA 598-617 AND BTW STA 617-636, X=-57 AT PAX COMPARTMENT. (CPAX) SUMMARY OF NRC 00390: CORROSION LEVEL 2. CUSP WEB (INNER AND UPPER SURFACE) BTW STA 503-522, BTW STA 54
- [SDR DALA2025013000728](https://openairdocs.org/sdr/DALA2025013000728.md): Skin · cracked · Apr 11, 2023 · N891AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN Y=1037, L13R TO L14R HAS CRACK REPAIR & INSPECTIONS. ACCOMPLISH ER/A 606978-14 REV A SECTION II INSPECTION WITHIN EVERY 15,000 CYCLES AFTER ACCOMPLISHMENT OF SECTION I REPAIR. ASSOCIATED ER/A 00-606978 ADDED FOR AC 9551. (LP #0786135)
- [SDR DALA2023041002745](https://openairdocs.org/sdr/DALA2023041002745.md): Unknown · unknown · Apr 10, 2023 · N891AT · Boeing 717200 · Fuselage Floor Panel
  > CORROSION ON FLOOR SUPPORT BTW STA Y=200 AND Y=223 X=15 AT PAX COMPARTMENT FLOOR STRUCTURE. (W1) SUMMARY OF NRC 00365: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=200 AND Y=223 X=15 AT PAX COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND B717-200 SRM 5
- [SDR DALA2023041002743](https://openairdocs.org/sdr/DALA2023041002743.md): Unknown · unknown · Apr 7, 2023 · N891AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON CUSP WEBS INNER AND UPPER SURFACE (4EA) BTW STA Y=433 AND STA Y=503, X=-57 AT PAX COMPARTMENT. (CPAX) SUMMARY OF NRC 00398: CORROSION LEVEL 2. CUSP WEB BTW STA Y=389 TO Y=503, X=-57 AT PAX COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP
- [SDR DALA2023041002740](https://openairdocs.org/sdr/DALA2023041002740.md): Unknown · unknown · Apr 7, 2023 · N891AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA 1037 BTW LONGERON 17LH AT CABIN PAX. SUMMARY OF NRC 00443: FRAME STA 1037 BTW LONGERON 17LH AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-20-07-2R REPAIR 4. (LP #2708504)
- [SDR DALA2023041002739](https://openairdocs.org/sdr/DALA2023041002739.md): Unknown · unknown · Apr 7, 2023 · N891AT · Boeing 717200 · Fuselage Floor Panel
  > SEVERAL CORROSION POINTS ON MEMBRANE BTW STA Y=155 AND Y=200 AND FROM X=-7 TO X=-44 AT PASSENGER COMPARTMENT FLOOR STRUCTURE. (W1). SUMMARY OF NRC 00358: CORROSION LEVEL 2. MEMBRANE BTW STA Y=155 AND Y=200 AND FROM X=-7 TO X=-44 WAS REPAIRED PER B717-200 SRM 5
- [SDR DALA2023040602680](https://openairdocs.org/sdr/DALA2023040602680.md): Unknown · unknown · Apr 5, 2023 · N891AT · Boeing 717200 · Fuselage Floor Panel
  > CRACKS ON PAN (INNER STRUCTURE) APROX BEAM 3 & BEAM 4 BTW STA Y=408 & Y=427 AND BEAM 5, BTW STA Y=408 & Y=427 OF AT FWD CARGO DOOR COMPARTMENT. SUMMARY OF NRC 00212: PAN (INNER STRUCTURE) APROX BEAM 3 & BEAM 4 BTW STA Y=408 & Y=427 AND BEAM 5, BTW STA Y=408 &
- [SDR DALA2023040602679](https://openairdocs.org/sdr/DALA2023040602679.md): Unknown · unknown · Apr 5, 2023 · N891AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON CUSP WEB BTW STA 927-946 AND ON STA 807 X-57. SUMMARY OF NRC 00522: CORROSION LEVEL 2. CUSP WEB BTW STA 927-946 AND ON STA 807 X-57 WAS REPAIRED PER B717-200 SRM 53-00-55 REPAIR 4. (LP #2705390)
- [SDR DALA2023040602678](https://openairdocs.org/sdr/DALA2023040602678.md): Unknown · unknown · Apr 4, 2023 · N891AT · Boeing 717200 · Fuselage Main, Frame
  > IN REF NRC 00384: CORROSION ON LH CUSP WEB BTW STA 746 TO 756, 636 TO 642, X:57. SUMMARY OF NRC 00521: CORROSION LEVEL 2. CUSP WEB BTW STA 746 TO 756, 636 TO 642, X:57 WAS REPAIRED PER B717-200 SRM 53-00-55 REPAIR 4. (LP #2704179)
- [SDR DALA2023040502675](https://openairdocs.org/sdr/DALA2023040502675.md): Unknown · undertorqued · Apr 4, 2023 · N891AT · Boeing 717200 · Fuselage Main, Frame
  > SECONDARY NRC, HIDDEN DAMAGE: CRACK ON CUSP WEB BTW STA Y=655-674 LH PASSENGER CABIN (CPAX). SUMMARY OF NRC 00490: CUSP WEB BTW STA Y=655-674 LH PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. (LP #2703902)
- [SDR DALA2023040402599](https://openairdocs.org/sdr/DALA2023040402599.md): Unknown · unknown · Apr 1, 2023 · N891AT · Boeing 717200 · Fuselage Floor Panel
  > CRACK ON PAN FWD UPPER SECTION AT L1 PASSENGER DOOR. SUMMARY OF NRC 00051: PAN ON FWD UPPER SECTION AT L1 PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R, REPAIR 3, PAR. 4, FIGURE 201. (LP #2698099)
- [SDR DALA2023040402598](https://openairdocs.org/sdr/DALA2023040402598.md): Unknown · unknown · Mar 31, 2023 · N891AT · Boeing 717200 · Fuselage Floor Panel
  > CRACK ON PAN (INNER STRUCTURE) APROX STA Y=370 & Y=389 BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00213: PAN (INNER STRUCTURE) APROX STA Y=370 & Y=389 BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R, REPAIR 1, PAR. 6, FIG. 201. (LP #2697134)

Next page: https://openairdocs.org/aircraft/N891AT/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N891AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N891AT/reports

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