# Service difficulty reports: N963AT

A list on [N963AT](https://openairdocs.org/aircraft/N963AT.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 4 · 196 reports

- [SDR DALA2026051903063](https://openairdocs.org/sdr/DALA2026051903063.md): Hinge Fitting · corroded · May 17, 2026 · N963AT · Boeing 717200 · Trailing Edge Flaps
  > CORROSION ON UPPER HOLES (2EAS) OF RH OUTBOARD WING FLAP HINGE FITTING ALSO CORROSION AND WEAR ON AFT OUTBOARD HINGE POINT (OUT FACE)OF SAME HINGE. RT OUTBOARD WING FLAP HINGE FITTING WAS REPAIRED PER CMM 27-50-5, PRI 634038-14 REV 6. & ER/A 634038-14 REV. (
- [SDR DALA2026051202974](https://openairdocs.org/sdr/DALA2026051202974.md): Spar Web · cracked · May 12, 2026 · N963AT · Boeing 717200 · Wing Spar
  > DURING TEST FLIGHT SPOILER ACTUATOR, CRACKED REAR SPAR WEB STA XRS=295-324 AT LT WING. REPAIRED PRI 633829-14 REV 8 AND ER/A 633829-14 (1589343) (AIRCRAFT GROUNDED)
- [SDR DALA2026051202973](https://openairdocs.org/sdr/DALA2026051202973.md): Skin · cracked · May 11, 2026 · N963AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED FUSELAGE SKIN BS 1076 AND LONG 15L. REPAIR AND PRI 633842-14 (1588945) (AIRCRAFT GROUNDED)
- [SDR DALA2026042902723](https://openairdocs.org/sdr/DALA2026042902723.md): Angle · cracked · Apr 24, 2026 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE ADJACENT TO FUSELAGE SKIN ON STA Y=1178 CANT AND LONG 17 LH SIDE. REPAIRED PER PRI 633860-14 (1561136) (AIRCRAFT GROUNDED)
- [SDR DALA2026031001643](https://openairdocs.org/sdr/DALA2026031001643.md): Valve · binding · Mar 8, 2026 · N963AT · Boeing 717200 · Engine Cooling System
  > SHIP 9522 CREW REPORTS STRONG DIRTY SOCK SMELL IN BACK OF AIRCRAFT. CORRECTIVE ACTION: FOUND #2 ENG SOURCE R/R #2 ENG BUFFER AIR VALVE FOUND IT BINDING & STIFF IN REF B717 AMM 75-22. CKS GOOD. (1485009)
- [SDR DALA2025082206255](https://openairdocs.org/sdr/DALA2025082206255.md): Latch · faulted · Aug 20, 2025 · N963AT · Boeing 717200 · Landing Gear Doors
  > ATB, PERFORMED AN AIR TURN BACK DUE TO A RIGHT MAIN LANDING GEAR UNSAFE LIGHT. REPLACED RT GEAR DOOR LATCH. OPS CHECK NORMAL.(7841530).
- [SDR DALA2024040103936](https://openairdocs.org/sdr/DALA2024040103936.md): Pan · cracked · Mar 29, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON INNER PAN (3 EA) NEAR BEAMS #5 & #3 FWD SIDE. ALSO NEAR BEAM #2 AFT SIDE AT FWD CARGO DOOR. ER/A 554100-14 REV. A SECTION I WAS ACCOMPLISHED. SUMMARY OF NRC 00097: FWD AND AFT INNER PAN BETWEEN BEAMS #1 AND BEAM #4 AT FWD CARGO DOOR WAS REPAIRED PER
- [SDR DALA2024040103935](https://openairdocs.org/sdr/DALA2024040103935.md): Hinge · obstructed · Mar 29, 2024 · N963AT · Boeing 717200 · Trailing Edge Flaps
  > INTERFERENCE BTW HEAD BOLT AND FWD OUTB FLAP HINGE AT RH WING. SUMMARY OF NRC 00808: FWD OUTB FLAP HINGE AT RH WING WAS REPAIRED PER ERA 616905-14 REV ORIGINAL SECTION I. ASSOCIATED ER/A 14-616905 ADDED FOR AC 9522. (LP #0268113)
- [SDR DALA2024032503738](https://openairdocs.org/sdr/DALA2024032503738.md): Bulkhead Web · cracked · Mar 25, 2024 · N963AT · Boeing 717200 · Fuselage Main, Bulkhead
  > CRACK ON WEB LH AND RH SIDE, (PROJECTION OF UPPER HINGE) AT AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR. SUMMARY OF NRC 00558: WEB AT AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. ALSO AFT CABIN
- [SDR DALA2024032303705](https://openairdocs.org/sdr/DALA2024032303705.md): Web · corroded · Mar 23, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB BTW Y=200 TO Y=208 X=56. SUMMARY OF NRC 00734: CORROSION LEVEL 2. CORROSION ON WEB BTW Y=200 TO Y=208 X=56 WAS REPAIRED PER PRI 616504-14 REV. 1 AND ERA 616504-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-616504 ADDED FOR AC
- [SDR DALA2024050805017](https://openairdocs.org/sdr/DALA2024050805017.md): Aileron · unknown · Mar 22, 2024 · N963AT · Boeing 717200 · Ailerons
  > -AD- PERFORM BALANCE PROCEDURE ON AILERON LH. SUMMARY OF NRC 00770: AILERON LH BALANCE PROCEDURE WAS PERFORMED PER B717-200 SRM 51-60-01-0G, ALSO AILERON LH WAS REMOVED / INSTALLED PER B717-200 AMM 27-10-01. ADJUSTMENT / TEST OK; AILERON CONTROL TAB L/H WAS RE
- [SDR DALA2024032203633](https://openairdocs.org/sdr/DALA2024032203633.md): Skin · corroded · Mar 21, 2024 · N963AT · Boeing 717200 · Entrance Stairs
  > CORROSION ON INTERNAL SKIN AND CUT OUT OF FWD AIR STAIRWELL DOOR. SUMMARY OF NRC 00109: FWD AIR STAIRWELL DOOR WAS REPLACED PER B717-200 AMM 52-63-01. (LP #0255910)
- [SDR DALA2024032203631](https://openairdocs.org/sdr/DALA2024032203631.md): Frame · cracked · Mar 21, 2024 · N963AT · Boeing 717200 · Fuselage Main, Frame
  > CRACK ON FRAME STA Y=1037 BTW LONG 14 RH AND 15 RH AT CABIN PAX. SUMMARY OF NRC 00386: FRAME STA Y=1037 BTW LONG 14 RH AND 15 RH AT CABIN PAX WAS REPAIRED PER ERA 616076-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 616076-14 REV 3. (LP #0255676)
- [SDR DALA2024032103584](https://openairdocs.org/sdr/DALA2024032103584.md): Longeron · corroded · Mar 19, 2024 · N963AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LONGERON END 25RH AT AFT CARGO COMPARTMENT C-2. SUMMARY OF NRC 00686: CORROSION LEVEL 2. LONGERON END 25RH AT AFT CARGO COMPARTMENT C-2 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0252387)
- [SDR DALA2024032103573](https://openairdocs.org/sdr/DALA2024032103573.md): Cusp Web · corroded · Mar 15, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION AT CUSP ANGLE WAS FOUND ON STA Y=200 AND X=54 - 60. SUMMARY OF NRC 00713: CUSP ANGLE WAS ON STA Y=200 AND X=54 - 60 REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 3 REPAIR 3. (LP #0246718)
- [SDR DALA2024031403330](https://openairdocs.org/sdr/DALA2024031403330.md): Skin · worn · Mar 14, 2024 · N963AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > WORN FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB). SUMMARY OF NRC 00013: FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB) WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 10 REPAIR 10. PERFORM VISUAL INSPECTION
- [SDR DALA2024031303282](https://openairdocs.org/sdr/DALA2024031303282.md): Skin · worn · Mar 13, 2024 · N963AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > WORN FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB). SUMMARY OF NRC 00013: FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB) WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 10 REPAIR 10. (LP #0242390)
- [SDR DALA2024031203223](https://openairdocs.org/sdr/DALA2024031203223.md): Floor Support · corroded · Mar 11, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OUT OF LIMITS AT FLOOR SUPPORT BTW STA Y=1022 AND STA Y=1060, ON X=44. SUMMARY OF NRC 00696: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1022 AND STA Y=1060, ON X=44 WAS REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0239946)
- [SDR DALA2024031103216](https://openairdocs.org/sdr/DALA2024031103216.md): Skin · dented · Mar 9, 2024 · N963AT · Boeing 717200 · Cargo/Baggage Doors
  > SEVERAL DENTS BTW 1 THRU 3 BEAMS AT AFT CARGO DOOR SKIN AND ALSO WORN SKIN AT AFT LWR DOOR SKIN CORNER. SUMMARY OF NRC 00016: OUTER SKIN AT AFT CARGO COMPARTMENT DOOR WAS FABRICATED AND REPLACED PER DWG 5910157 REV CW AND B717-200 SRM 51-41-02-0G. (LP #0237570
- [SDR DALA2024031103215](https://openairdocs.org/sdr/DALA2024031103215.md): Cusp Web · corroded · Mar 8, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB BTW STA Y986 TO STA Y1000 X=-60 AT CPAX. STRUCTURE WAS MEASURED WITH AN ORIGINAL THICKNESS OF 0.020IN. REMAINING THICKNESS IS 0.005IN THEREFORE REWORKED AREA IS OUT OF LIMITS. SUMMARY OF NRC 00697: CORROSION LEVEL 2. CUSP WEB BTW STA Y986
- [SDR DALA2024031103214](https://openairdocs.org/sdr/DALA2024031103214.md): Cusp Web · corroded · Mar 8, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON CUSP WEB BTW STA Y408 AND X=- 60 AT CPAX. SUMMARY OF NRC 00569: CORROSION LEVEL 2. CUSP WEB BTW STA Y408 AND X=-60 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0235862)
- [SDR DALA2024030803182](https://openairdocs.org/sdr/DALA2024030803182.md): Intercostal · corroded · Mar 7, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL BTW STA 636 TO 653 AND BTW LONGERONS 27-L TO 28-L AT FWD CC. SUMMARY OF NRC 00316: CORROSION LEVEL 2. INTERCOSTAL ON BTW STA 636 TO 653 AND BTW LONGERONS 27-L TO 28-L AT FWD CC WAS REPLACED PER B717 SRM 51-40-02-0G. (LP #0234436)
- [SDR DALA2024030603064](https://openairdocs.org/sdr/DALA2024030603064.md): Web · corroded · Mar 6, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND AT DIAPHRAGM BEETWEN STA Y=198 AND X=54 (PASSENGER DOOR ENTRANCE). SUMMARY OF NRC 00616: CORROSION LEVEL 2. DIAPHRAGM BEETWEN STA Y=198 AND X=54 (PASSENGER DOOR ENTRANCE) WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2 PAR 4
- [SDR DALA2024030503010](https://openairdocs.org/sdr/DALA2024030503010.md): Intercostal · cracked · Mar 4, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR. SUMMARY OF NRC 00059: INTERCOSTAL OF MECHANISM BTW BEAM #4 AND BEAM #5 OF L1 DOOR WAS FABRICATED AND REPLACED PER DWG 9955763 REV L, B717-200 SRM 51-41-01-0G AND 51-41-02-0G. (LP #0229988)
- [SDR DALA2024030603063](https://openairdocs.org/sdr/DALA2024030603063.md): Skin · cracked · Mar 3, 2024 · N963AT · Boeing 717200 · Cargo/Baggage Doors
  > CRACK ON INTERNAL SKIN NEAR TO BEAM #3 FWD EDGE WAS FOUND AT FWD CARGO DOOR. SUMMARY OF NRC 00745: INTERNAL SKIN NEAR TO BEAM #3 FWD EDGE AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 3 REPAIR 3, FIGURE 201. (LP #0231760)
- [SDR DALA2024030503004](https://openairdocs.org/sdr/DALA2024030503004.md): Tab · dented · Mar 2, 2024 · N963AT · Boeing 717200 · Rudder, Tab Structure
  > SEVERAL DENTS ON RH SIDE OF RUDDER CONTROL TAB. SUMMARY OF NRC 00081: SEVERAL DENTS ON RH SIDE OF RUDDER CONTROL TAB WERE MEASURED AND FOUND WITH NO DISBONDS AND ARE WITHIN LIMITS PER B717-200 SRM 55-41-01-1A PROCEDURE I ALLOWABLE DAMAGE I PAR 3,A,(4),(C), AND
- [SDR DALA2024030402939](https://openairdocs.org/sdr/DALA2024030402939.md): Cusp Web · corroded · Mar 2, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK CUSP WEB RH LOWER AREA STA 696 CPAX. SUMMARY OF NRC 0547: CUSP WEB RH ON STA 655 TO STA 715 WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4, 51-41-02-0G, AND 51-41-05-0G. PERFORM A GVI EVERY "C" CHECK PER B717-200 SRM 53-00-55-2R-4 REPAIR 4, PAR 6.
- [SDR DALA2024030402936](https://openairdocs.org/sdr/DALA2024030402936.md): Floor Support · corroded · Mar 2, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT ON STA Y=200 BTW X=-44 AND X=-55 AT PAX COMPARTMENT. (W1). SUMMARY OF NRC 00553: CORROSION LEVEL 2. DUE TO EXCESS CORROSION (EXFOLIATION), FLOOR SUPPORT ON STA Y=200 BTW X=-44 AND X=-55 AT PAX COMPARTMENT (W1) WAS REPLACED PER DWG 99
- [SDR DALA2024030402933](https://openairdocs.org/sdr/DALA2024030402933.md): Web · corroded · Mar 1, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON MEMBRANE STA Y=201 BTW X=11 TO X=-44 AT PAX COMPARTMENT. (W1). CORROSION LEVEL 2. MEMBRANE STA Y=201 BTW X=11 TO X=-44 AT PAX COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R, PROCEDURE 2 REPAIR 2. (LP #0225731)
- [SDR DALA2024022902795](https://openairdocs.org/sdr/DALA2024022902795.md): Web · corroded · Feb 28, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON MEMBRANE STA Y=178 AND BTW X=-2 AND X=-26 AT PASSENGER COMPARTMENT (W1). SUMMARY OF NRC 0551: CORROSION LEVEL 2. MEMBRANE STA Y=178 AND BTW X=-2 AND X=-26 AT PASSENGER COMPARTMENT (W1) WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 2. (LP #02225
- [SDR DALA2024022902794](https://openairdocs.org/sdr/DALA2024022902794.md): Cusp Web · corroded · Feb 28, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION AT CUSP WEB BETWEN STA 832 AND STA 851 AND X=60 PAX CABIN. SUMMARY OF NRC 0395: CORROSION LEVEL 2. CORROSION AT CUSP WEB BETWEN STA 832 AND STA 851 AND X=60 PAX CABIN WAS REMOVED B717-200 SRM 51-10-04-0G PAR 26 C (1). (UT) THICKNESS MEASUREMENT WAS A
- [SDR DALA2024022802763](https://openairdocs.org/sdr/DALA2024022802763.md): Cusp Web · cracked · Feb 27, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON CUSP WEB (LOWER AREA) BTW STA 1017 TO STA 1020 AND X=45 AT CPAX. SUMMARY OF NRC 00589: CUSP WEB (LOWER AREA) BTW STA 1017 TO STA 1020 AND X=45 AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PRCEDURE 4 REPAIR 4. (LP #0221152)
- [SDR DALA2024022602642](https://openairdocs.org/sdr/DALA2024022602642.md): Door Frame · corroded · Feb 25, 2024 · N963AT · Boeing 717200 · Fuselage Main, Structure
  > EXFOLIATION CORROSION AT AFT CARGO LWR DOOR JAMB FROM STA Y=954 TO Y=996. SUMMARY OF NRC 00020: CORROSION LEVEL 2. AFT CARGO LWR DOOR JAMB FROM STA Y=954 TO Y=996 WAS REPLACED PER B717 SRM 53-20-15-2R REPAIR 7, 51-41-02-0G, AND 51-41-04-0G. (LP #0218389)
- [SDR DALA2024022602640](https://openairdocs.org/sdr/DALA2024022602640.md): Longeron · corroded · Feb 25, 2024 · N963AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION AT STA 130 APROX AND L30 COMPARTMENT E&E. SUMMARY OF NRC 00225: CORROSION LEVEL 2. LONGERON 30 STA Y=110 TO Y=130 WAS REPLACED PER DWG 5411401 REV DT AND B717-200 SRM 51-41-02-0G. (LP #0217998)
- [SDR DALA2024022202461](https://openairdocs.org/sdr/DALA2024022202461.md): Floorbeam · corroded · Feb 21, 2024 · N963AT · Boeing 717200 · Fuselage Main, Floor Beam
  > CORROSION ON ANGLE OF FLOOR STRUCTURE STA Y=1053 X=20 AT CABIN PAX. SUMMARY OF NRC 00374: CORROSION LEVEL 2. ANGLE OF FLOOR STRUCTURE STA Y=1053 X=20 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0212052)
- [SDR DALA2024022002326](https://openairdocs.org/sdr/DALA2024022002326.md): Frame · cracked · Feb 20, 2024 · N963AT · Boeing 717200 · Fuselage Main, Frame
  > CRACKED FRAME ON STA Y=715 BTW S-27L AND S-28L AT CANTED KEEL BEAM AREA. (FUS) SUMMARY OF NRC 0549: CRACKED FRAME ON STA Y=715 BTW S-27L AND S-28L AT CANTED KEEL BEAM AREA WAS REPAIRED PER B-717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. PERFORM AN EXTERNAL GVI
- [SDR DALA2024022002322](https://openairdocs.org/sdr/DALA2024022002322.md): Floor Support · cracked · Feb 17, 2024 · N963AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT STA 636 X=0 AND Z=-2 AT FWD CC. SUMMARY OF NRC 00309: FLOOR SUPPORT (INTERCOSTAL) STA 636 X=0 AND Z=-2 AT FWD CARGO WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP #0205320)
- [SDR DALA2023080406303](https://openairdocs.org/sdr/DALA2023080406303.md): Unknown · unknown · Aug 3, 2023 · N963AT · Boeing 717200 · Emergency Lighting
  > THE CENTER AISLE OVERHEAD RED EXIT SIGN IS BROKEN AND MISSING THE BACK HALF OF THE SIGN. MAINTENANCE REPLACED THE SIGNAGE. OPERATIONAL CHECK OF THE SIGN WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #4398332)
- [SDR DALA2023060204427](https://openairdocs.org/sdr/DALA2023060204427.md): Unknown · unknown · Jun 1, 2023 · N963AT · Boeing 717200 · Electrical Power System
  > SHIP 9522 -MISC/DE- DURING APPROACH FOR LANDING, THE "BUS DC R OFF" INDICATION ILLUMINATED. WHICH WAS FOLLOWED BY 15 OTHER DISCREPANCY INDICATIONS. THE QRH WAS COMPLIED WITH AND THE CREW DECLARED EMERGENCY DUE TO THE IMPENDING NO FLAP AND NO SLAT LANDING. A HO
- [SDR DALA2022081605533](https://openairdocs.org/sdr/DALA2022081605533.md): None · none · Aug 14, 2022 · N963AT · Boeing 717200 · Hydraulic System, Main
  > SHIP 9522 -HYD/GEAR- THE AIRCRAFT EXPERIENCED A BIRD STRIKE WHICH DAMAGED HYDRAULIC LINES AND DUE TO THAT DAMAGE, LOSS FLUID OUT OF THE RIGHT HYDRAULIC SYSTEM. AN ALTERNATE GEAR EXTENSION WAS REQUIRED TO LOWER THE LANDING GEAR. AN EMERGENCY WAS DECLARED FOR TH
- [SDR DALA2022052403549](https://openairdocs.org/sdr/DALA2022052403549.md): Light · unserviceable · May 23, 2022 · N963AT · Boeing 717200 · Emergency Lighting
  > THE EVACUATION EXTERIOR EMERGENCY LIGHTS ON BOTH SIDES ARE INOPERATIVE. TRANSFER TO MEL 33-51-02A. NEEDS BATTERY. REPLACED OVERWING EMERGENCY LIGHT AND POWER SUPPLY BATTERY PER B717 AMM 33-51-06. NO HELP. REPLACED OVERWING EMERGENCY LIGHT POWER RELAY R2-273 PE
- [SDR DALA2022052403548](https://openairdocs.org/sdr/DALA2022052403548.md): Skin · cracked · May 20, 2022 · N963AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1022 BTW LONG 13RH-14 RH (FUS). SUMMARY OF NRC 00029: FUSELAGE SKIN STA Y=1022 WAS REPAIRED PER PRI 599215-14 REV. 2 AND ER/A 599215-14 REV ORIGINAL SECTION I: PERMANENET REPAIR. ACCOMPLISH REPETITIVE INSPECTION WITHIN EV
- [SDR DALA2022052003455](https://openairdocs.org/sdr/DALA2022052003455.md): Frame · corroded · May 19, 2022 · N963AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON FRAME CLIP STA Y=927 BTW LONG 27LH TO 28RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00191: CORROSION LEVEL 2, FRAME CLIP STA Y=927 BTW LONG 27LH TO 28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G, SRM 51-41-05-0G. (LP #2242428)
- [SDR DALA2022052003454](https://openairdocs.org/sdr/DALA2022052003454.md): Track · corroded · May 19, 2022 · N963AT · Boeing 717200 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH TIE TRACK BTW STA Y=896-954 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00098: CORROSION LEVEL 2, TIE TRACK WAS REPLACED PER B717 SRM 51-41-01-0G BECAUSE IT IS OUT OF LIMITS PER B717 SRM-53-20-52-1A-2 PAR 4 FIG 101 AND B717 DC-MD/BOEING NDT MANUAL
- [SDR DALA2022052003457](https://openairdocs.org/sdr/DALA2022052003457.md): Battery Pack · inoperative · May 18, 2022 · N963AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > ER/A 599216-14, FUSELAGE SKIN AT Y=1076 AND Y=1087, L-13R TO L-14R HAS CRACKS. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTIONS. ACCOMPLISH ER/A 599216-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 24 MONTH INTERVAL AFTER 17MAY22. ASSOCIATED ER/A 1
- [SDR DALA2022051903434](https://openairdocs.org/sdr/DALA2022051903434.md): None · none · May 18, 2022 · N963AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKS ON EXTERNAL FUSELAGE SKIN STA Y=1076 AND Y=1087 BTW LONG 13RH-14RH (FUS). SUMMARY OF NRC 00030: EXTERNAL FUSELAGE SKIN STA Y=1076 AND Y=1087 BTW LONG 13RH-14RH WAS REPAIRED PER ER/A 599216-14 REV. ORIGINAL SECTION L: PERMANENT REPAIR AND PRI 599216-14 R
- [SDR DALA2022051803423](https://openairdocs.org/sdr/DALA2022051803423.md): None · none · May 17, 2022 · N963AT · Boeing 717200 · Fuselage Main, Frame
  > CORROSION ON FRAME CLIP STA Y=908 BTW LONG 28LH TO 28 RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00190: LEVEL CORROSION 2, FRAME CLIP STA Y=908 BTW LONG 28LH TO 28 RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2239592)
- [SDR DALA2022051703372](https://openairdocs.org/sdr/DALA2022051703372.md): Skin · debonded · May 17, 2022 · N963AT · Boeing 717200 · Trailing Edge Flaps
  > DISBOND (0.700 IN LENGTH X 0.700 IN WIDTH) ON RHS I/B FIXED VANE, UPPER SKIN 60.5 IN FROM I/B END AND 5.5 IN FROM T/E. SUMMARY OF NRC 00317: INBOARD FIXED VANE, UPPER SKIN AT RH WING WAS REPAIRED PER B-717-200 SRM 51-70-02-0G PROCEDURE GENERAL IN REFERENCE OF
- [SDR DALA2022051703371](https://openairdocs.org/sdr/DALA2022051703371.md): Skin · debonded · May 17, 2022 · N963AT · Boeing 717200 · Trailing Edge Flaps
  > IN REF NRC 00116: ONE DISBOND WAS FOUND ON DENT STA XV1=143 OF 1.500 IN X 1.100 IN LENGTH / WIDTH ON INBOARD FIXED VANE UPPER SKIN AT LH WING. SUMMARY OF NRC 00311: INBOARD FIXED VANE UPPER SKIN AT LH WING WAS REPAIRED PER B-717-200 SRM 51-70-02-0G PROCEDURE G
- [SDR DALA2022051603339](https://openairdocs.org/sdr/DALA2022051603339.md): None · none · May 16, 2022 · N963AT · Boeing 717200 · Passenger/Crew Doors
  > CRACK ON BEAM #1 STA=160 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00089: BEAM #1, STA=160 AT PASSENGER ENTRANCE DOOR (L1) WAS REPAIRED PER B-717 SRM 52-10-02-2R REPAIR 7. (LP #2237275)

Next page: https://openairdocs.org/aircraft/N963AT/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 = 'N963AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N963AT/reports

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