# Service difficulty reports: JASC 2797

A list on [JASC 2797](https://openairdocs.org/jasc/2797.md).

Reports filed under 2797 · Flight Control System Wiring, newest first.

Page 1 of 19 · 919 reports

- [SDR SIMA20261009001](https://openairdocs.org/sdr/SIMA20261009001.md): Wire Harness · faulted · Oct 9, 2026 · N746CC · Emb ERJ170100LR
  > SLAT FAIL IN FLIGHT. SLAT FAIL AT 0. FLAPS WORKED AS NORMAL. SHAKER ANTICIPATED. EMERGENCY DECLARED. RAR RH WING INBD SLAT HARNESS W611 IAW E170 AMM 27-83-07. OPS CHECK GOOD. REF NRWC 746-ORD-02963.
- [SDR DALA2026092805379](https://openairdocs.org/sdr/DALA2026092805379.md): Wire · damaged · Sep 19, 2026 · N583NW · Boeing 757351
  > DIVERTED TO MSP DUE L/E SLAT ASYMMETRY MESSAGE. REPAIRED WIRE W8526-1001-20 OF LEFT WING TO SLAT LOSS SWITCH. (AIRCRAFT GROUNDED)
- [SDR SCNA20260917401](https://openairdocs.org/sdr/SCNA20260917401.md): Elec Connector · loose · Sep 13, 2026 · N5237A · Boeing 737800*
  > DURING LANDING CHECKLIST NOTICED THAT THE SPEED BRAKE ARM LIGHT DID NOT ILLUMINATE AFTER ARMING THE SPEED BRAKE. MOVED LEVER BACK DOWN AND BACK TO ARM, ALSO DID A LAMP CHECK AND ARM LIGHT AND DO NOT ARM WOULDN'T ILLUMINATE. AFTER LANDING NOTICED AUTO SPEED BRA
- [SDR SWAA2026082712675](https://openairdocs.org/sdr/SWAA2026082712675.md): Wire · damaged · Aug 26, 2026 · N8543Z · Boeing 7378H4
  > DURNING APPROACH WHEN SELECTING FLAPS 15 LE FLAPS IN TRANSIT ILLUMINATED DURNING APPROACH WHEN SELECTING FLAPS 15 LE FLAPS IN TRANSIT ILLUMINATED REPAIRED WIRE W6588-2202B-20 APPROX 6 FROM D39939 PER SWPM 20-10-13 AND WDM 27-81-21. OPS CHECK GOOD PER AMM 27-81
- [SDR VNAA2026081722802](https://openairdocs.org/sdr/VNAA2026081722802.md): Ecu · unserviceable · Aug 16, 2026 · N599NN · Cndair CL6002D24
  > STAB/ MACH TRIM CAUTION IN FLIGHT AND SLATS/FLAPS HALFSPEED / REMOVED AND REPLACED SFECU 1 IAW CRJ 900 AMM 27-51-06-400-801 OPS CK GOOD
- [SDR SWIA2026072976703](https://openairdocs.org/sdr/SWIA2026072976703.md): Elec Connector · corroded · Jul 29, 2026 · N712SK · Cndair CL6002C11
  > FLAPS FAIL CAUTION MESSAGE AT CRUISE, COMPLIED WITH QRH FOR A FLAPS 0 LANDING. BRAKES 2672 AT GATE. (FLIGHT 3702) REF AML 1952370, REF AML 1952385. TROUBLESHOT REPEAT FLAP FAIL MSG WITH ACFT HARD FAIL. FOUND REPEAT MSG FOR RT BPSU RESOLVER FLAGGED IN MDC.
- [SDR DALA2026071004068](https://openairdocs.org/sdr/DALA2026071004068.md): Elec Connector · contaminated · Jul 9, 2026 · N663DN · Boeing 757232
  > DE/FCNT-DUE TO FLAP ISLN VALVE EICAS MESSAGE. REPLACED RELAY K10104 IN P33. FLAP BYPASS VALVBE ELEC CONNECTOR FOUND TO BE FULL OF HYD FLUID AND OTHER DEBRIS. CLEANED AND RECONNECTED. SLAT DRIVE MOTOR CONNECTOR FOUND LOOSE. INSPECTED AND REINSTALLED. OPS CHEC
- [SDR SWAA2026050495240](https://openairdocs.org/sdr/SWAA2026050495240.md): Connector · dirty · May 3, 2026 · N7831B · Boeing 7377CT
  > AFTER ROTATION (155KTS) TAKE OFF CONFIG WARNING LIGHT AND HORN ON AND WENT OUT AFTER LIFT OFF. GEAR UP NORMALLY. FLAPS WOULD NOT RETRACT AND INDICATED LESS THAN 1. NO ASSYMERTY. ALL FLAP EXTENSION ACCOMPLISHED NORMALLY AFTER LANDING #6 SLAT INDICATION LIGHT I
- [SDR DALA2026050102778](https://openairdocs.org/sdr/DALA2026050102778.md): Receptacle · corroded · Apr 29, 2026 · N336NW · Airbus A320212
  > CORROSION ON ELECTRICAL RECEPTACLES (7540 VC) (7542 VC) ON RH WING (REFER TO RII AMDS CARD 2751-9202). REPLACED ELECTRICAL RECEPTACLES (7540 VC) (7542 VC) ON RT WING IAW AIRBUS ESPM 20-56-42 PAGEBLOCK 0301 CONFIG 01, AIRBUS ESPM 20-44-11 PAGEBLOCK 0101 CONFIG
- [SDR SWAA2026040786777](https://openairdocs.org/sdr/SWAA2026040786777.md): Circuit Breaker · incorrect · Apr 6, 2026 · N8749Q · Boeing 7378
  > ON SHORT FINAL; FLAPS SELECTED TO 5 WITH NO FLAP MOVEMENT. RAN QRH AND ALTN FLAPS USED FOR LANDING. FOUND C/B P6-2 A12 POPPED. RESET C/B AND C/B STAYS IN.<[01] FOUND C/B C213 (FC TE FLAP POS/SKEW SNSR & IND LEFT) AT P6-2 A12 TO BE IN AND REMAINS IN. FOUND MAIN
- [SDR DALA2026031301761](https://openairdocs.org/sdr/DALA2026031301761.md): Wire · disconnected · Mar 12, 2026 · N696DL · Boeing 757232
  > ATO- DUE TO SPOILERS TAKEOFF CONFIG WARNING MESSAGE. FOUND PIN/WIRE DISCONNECTED FROM S371 AND REPAIRED SAME. S493 REMOVED AND REPLACED. INSTALLED PINS ON TB190. (AIRCRAFT GROUNDED)
- [SDR AALA202601219260](https://openairdocs.org/sdr/AALA202601219260.md): Circuit Breaker · tripped · Jan 19, 2026 · N964NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: STAB TRIM CIRCUIT BREAKER FOUND POPPED ON CLIMB OUT. AIRCRAFT EMERGENCY LANDED SAFELY AT LAX. CHECKED PER FIM 27-41-00-810-805 RESET AFCS STAB TRIM CIRCUIT BREAKER, PER AMM 27-41-00. PERFORMED STAB TRIM
- [SDR SIMA20260116001](https://openairdocs.org/sdr/SIMA20260116001.md): Wire Harness · failed · Jan 16, 2026 · N267NN · Emb ERJ170200LR
  > SLAT FAIL ON APPRCH DECLARED EMERGENCY. RAR SLAT 3/4 LH HARNESS IAW AMM 27-83-07. OPS CECKED IAW AMM 27-80-00-710-801-A/500. OPS CHECKED GOOD.
- [SDR AALA202601140298](https://openairdocs.org/sdr/AALA202601140298.md): Elec Connector · faulted · Jan 13, 2026 · N899NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING APPROACH FLAP GAGE SHOWED FLAP ASYMMETRICINDICATION, CYCLED HANDLE BUT NO MOVMENT ON THE GAGE. AIRCRAFT EMERGENCY LANDED SAFELY AT ORD. REMOVE AND REPLACED NUMBER 5 INBOARD FLAP INBOARD SKEW SENSO
- [SDR ABXA20260108006](https://openairdocs.org/sdr/ABXA20260108006.md): Elec Connector · dirty · Jan 8, 2026 · N390CM · Boeing 767381
  > DURIING TAXI OUT, TE FLAP DISAGREE CAUTION AND TRAILING EDGE LIGHT UPON SELECTION OF FLAPS 5 FOR TAKEOFF. AIRCRAFT RETURNED TO BLOCKS. (BTB). TROUBLESHOOT TO MANUAL OVERRIDE BYPASS VALVE STUCK OPEN. CLEANED THE ELECTRICAL CONNECTOR AND CYCLED LEVER MULTIPLE
- [SDR U5QA202512220165](https://openairdocs.org/sdr/U5QA202512220165.md): Wire · broken · Dec 22, 2025 · N151JE · Gulstm GIVXG450
  > LATERAL CONTROL HYD. OFF AMBER MESSAGE REPOSTED DURING MAINTENANCE CHECK FLIGHT. FOUND BOTH WIRES OF TWISTED SHIELDED PAIR FROM AIRFRAME TO FORCE LINK SENSOR BROKEN AT ADEL CLAMP AT LH AILERON ACTUATOR. CRIMPED ON NEW SPLICES/ENVIRONMENTAL SEALS. REFERENCE G4
- [SDR DALA2025111808408](https://openairdocs.org/sdr/DALA2025111808408.md): Elec Connector · worn · Nov 16, 2025 · N363NB · Airbus A319114
  > WEAR ELECTRICAL CONNECTOR RECEPTACLES (2 EA) (FIN 7543VC AND 7541VC) A ND PROXIMITY SENSOR CONNECTORS (2 EA) (FIN 37CV AND 39CV) ON INTERCONNECTING STRUT I/B FLAP LH WING. CORRECTIVE ACTION: R/R ELECTRICAL CONNECTOR RECEPTACLES (2 EA) (FIN 7543VC AND 7541VC) A
- [SDR DALA2025111208290](https://openairdocs.org/sdr/DALA2025111208290.md): Elec Connector · broken · Nov 11, 2025 · N353NB · Airbus A319114
  > BROKEN ELECTRICAL CONNECTOR (31CE10A) LOC. ON SPOILER ACTUATOR 5 RH WING. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR (31CE10A) LOC. ON SPOILER ACTUATOR #5 RH WING AS PER AIRBUS ESPM 20-44-11. (1299225).
- [SDR DALA2025111008206](https://openairdocs.org/sdr/DALA2025111008206.md): Elec Connector · corroded · Nov 9, 2025 · N353NB · Airbus A319114
  > CORROSION ON ELECTRICAL CONNECTOR 16CA LOCATED ARTIFICIAL FEEL AND RUD DER TRAVEL LIMITING AT VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR (16CA-A) AS PER AIRBUS ESPM 20-44- 11. (1295830).
- [SDR DALA2025111008204](https://openairdocs.org/sdr/DALA2025111008204.md): Elec Connector · corroded · Nov 9, 2025 · N353NB · Airbus A319114
  > CORROSION ELECTRICAL CONNECTOR ON IB ELEVATOR SERVO CONTROL ACTUATOR (1E/A) AND OB ELEVATOR SERVO CONTROL ACTUATOR (2E/A) ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTORS (34CE3-C) (34CE3-A) (34CE1-C) AS PER AIRBUS ESPM 20-44-11.
- [SDR CALA2025110510908](https://openairdocs.org/sdr/CALA2025110510908.md): Elec Connector · shorted · Nov 5, 2025 · N27539 · Boeing 7379
  > TECH SUPPORT UPDATE ON CHRONIC MX AND SPOILER LIGHT W/AHM LOGGING FAULT 27-01620 A COUPLE TIMES SPOILER 9 NOT FOLLOWING COMMANDED SIGNAL FROM SCE. PERF FIM TASK 27-61-T850 DO THE WIRING CHKS FROM SCE TO 9 SPOILER PCU SHAKE HARNESS DOWN WHERE POSSIBLE ENSURE G
- [SDR DALA2025090106452](https://openairdocs.org/sdr/DALA2025090106452.md): Elec Connector · worn · Aug 30, 2025 · N357NB · Airbus A319114
  > WORN ELECTRICAL CONNECTOR 7540VC ON I/B FLAP RT. REPLACED ELECTRICAL CONNECTOR 7540VC ON I/B FLAP RT IAW AIRBUS ESPM 20-44-11. (1172999).
- [SDR DALA2025082906405](https://openairdocs.org/sdr/DALA2025082906405.md): Elec Connector · corroded · Aug 28, 2025 · N357NB · Airbus A319114
  > CORROSION ELECTRICAL CONNECTORS SPOILER 2,3,4 AND 5 ACTUATOR OF ON LH WING. REPLACED ELECTRICAL CONNECTORS SPOILER #2, 3, 4 AND 5 ACTUATOR OF LH WING AS PER AIRBUS ESPM 20-44-11. (1169860).
- [SDR DALA2025082506316](https://openairdocs.org/sdr/DALA2025082506316.md): Elec Connector · corroded · Aug 21, 2025 · N355NB · Airbus A319114
  > CORROSION ON ELECTRICAL CONNECTORS 7541VC AND 7543VC OF INTERCONNECTING STRUT ON LH WING. REPLACED ELECTRICAL CONNECTORS 7541VC AND 7543VC OF INTERCONNECTING STRUT ON LH WING AS PER AIRBUS ESPM 20-44-11. (1156567).
- [SDR JJBA20250822045](https://openairdocs.org/sdr/JJBA20250822045.md): Elec Connector · faulted · Aug 18, 2025 · N17138 · Emb EMB145XR
  > FLAP FAIL, SPS ADVANCED EICAS MESSAGE DISPLAYED AFTER MOVING FLAP HANDLE DURING APPROACH. REMOVED AND REPLACED ELECTRICAL CONNECTOR PLUG P1104. FLAPS OPS CHECK GOOD. PERFORMED FLAP SCREWJACK ACTUATOR LUBRICATION ON ALL FLAP ACTUATORS. PERFORMED FLAP SCREWJACK
- [SDR DALA2025081206035](https://openairdocs.org/sdr/DALA2025081206035.md): Elec Connector · corroded · Aug 11, 2025 · N346NB · Airbus A319114
  > SHIP 3146 EMPENNAGE VERTICAL STABILIZER T/E AREA, RUDDER POSITION UNIT 42WV ELECTRICAL CONNECTOR WITH CORROSION. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTORS IAW ESPM REF 20-44-11. (1137635).
- [SDR DALA2025080105794](https://openairdocs.org/sdr/DALA2025080105794.md): Wire · damaged · Jul 31, 2025 · N358NW · Airbus A320212
  > ATB DUE TO THE FLAPS BEING LOCKED BETWEEN POSITION 1 AND 2 WITH A FLAPS FAULT MESSAGE. REPLACED PIN ON WIRE 2751-5907R, REPLACED CONNECTOR 7505VC-B AND REPLACED PROX SENSOR 37CV.
- [SDR UIEA2025072901053](https://openairdocs.org/sdr/UIEA2025072901053.md): Elec Connector · damaged · Jul 29, 2025 · N645GT · Boeing 767324
  > CONFIG WARNING AND FLAPS AFTER CLEAN UP. NOSE GEAR EXTENSION EXPERIENCED A LOUD BANG. SPD LIM MESSAGE NEXT TO 250 KNOTS ON SPEED TAPE WITH FLAPS UP. RESEATED PUSHED BACK ELEC CONNECTOR D1756 PIN 2 IAW SWPM 20-61-00, NO FURTHER DEFECTS NOTED.
- [SDR 3EJA202508150003](https://openairdocs.org/sdr/3EJA202508150003.md): Elec Connector · not seated · Jul 9, 2025 · N853JS · Cessna 560XL
  > ON APPROACH AND GIVEN INSTRUCTION TO SLOW. CONFIGURED THE AIRPLANE FOR FLAPS 15. RECEIVED A STAB MISCOMPARE & DISCONTINUED THE APPROACH. REMOVED, INSPECTED & REINSTALLED PCBS NZ016 AND NZ017. CLEANED AND INSPECTED ELECTRICAL CONNECTOR PF029, RESEATED ELECTRI
- [SDR AALA202507086655](https://openairdocs.org/sdr/AALA202507086655.md): Elec Connector · failed · Jul 4, 2025 · N815NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: DURING CLIMB THE AIRCRAFT PITCHED UP AND DOWN WITH THE LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT PHL. FOUND PIN 34 OF CONNECTOR DM22 TO HAVE LOW
- [SDR HNAA2025062400460](https://openairdocs.org/sdr/HNAA2025062400460.md): Elec Connector · loose · Jun 23, 2025 · N905JH · Emb EMB145LR
  > LOW SPEED REJECTED TAKEOFF AT 20 KNOTS DUE TO OPEN SPOILER INDICATION ON EICAS AND UNCOMMANDED PITCH TRIM MOVEMENT, UP 9 DOWN 4 FACT 23JUN25 23:04 CLT INSPECTED SPOILER SYSTEM AND FOUND LH OB SPOILER PROX SWITCH CONNECTOR PLUG LOOSE AND WOULD NOT STAY T
- [SDR DALA2025061204465](https://openairdocs.org/sdr/DALA2025061204465.md): Wire · damaged · May 27, 2025 · N1604R · Boeing 767332
  > SHIP 1604 -DE/MISC- DUE TO LE ASYM INDICATION IN FLIGHT. CORRECTIVE ACTION: REPLACED SWITCH S286 AND REPAIRED WIRE ON CONNECTER D4434J. ALL CHECKED NORMAL.
- [SDR AALA202505285710](https://openairdocs.org/sdr/AALA202505285710.md): Elec Connector · shorted · May 26, 2025 · N954AN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: AT TAKEOFF ROTATION, THE TAKE OFF CONFIGURATION WARNING HORN SOUNDED. THE HORN SILENCED SHORTLY AFTER, HOWEVER THE FLAPS WOULD NOT RESPOND HYDRAULICALLY TO FLAP HANDLE MOVEMENT. THE FLAPS REMAINED IN TAK
- [SDR SWAA2025051971039](https://openairdocs.org/sdr/SWAA2025051971039.md): Motor · burned out · May 13, 2025 · N259WN · Boeing 7377H4
  > F.O. STICK SHAKER SHORT CIRCUIT; BURNT WIRES/SMOKE ON CAPT PREFLIGHT TEST.<[01] R&R FO?S STICK SHAKER MOTOR AND CONNECTOR IAW 27-32-31.
- [SDR CALA2025051304648](https://openairdocs.org/sdr/CALA2025051304648.md): Elec Connector · damaged · May 10, 2025 · N26208 · Boeing 737824
  > SPLIT FLAP ON ARRIVAL. LEFT FLAP LESS THAN ONE RIGHT FLAP STUCK AT ZERO. PILOT INFOMED THAT THEY SELECTED FLAPS ONE THE RH SIDE FLAPS DROPPED AND THE LH FLAPS STAYED THE SAME THE SAW SPLIT FLAPS AND DID THE SPILT FLAPS PROCEDURE. THEY ARMED ALTERNATE FLAPS AN
- [SDR 2025FA0000378](https://openairdocs.org/sdr/2025FA0000378.md): Elec Connector · unsecure · May 8, 2025 · N824NE · Cessna 525C
  > DURING CLIMB, WITH AUTOPILOT ENGAGED, CREW WAS ALERTED TO A RT WING OVERTEMP MESSAGE, FOLLOWED BY AUTOPILOT DOING UNCOMMANDED LT & RT ROLLS RAPIDLY, AUTOPILOT DISENGAGED BY CREW & THE ACFT FLOWN BY HAND. CREW NOTED THAT THE AILERON TRIM INDICATED FULL LT DEFL
- [SDR SWAA2025042126532](https://openairdocs.org/sdr/SWAA2025042126532.md): Elec Connector · dirty · Apr 20, 2025 · N286WN · Boeing 7377H4
  > WITH LAP LEVER TO 25; FLAP INDICATOR SHOWED SPLIT FLAP CONDITION WITH 1 NEEDLE AT 0 AND THE OTHER AT.5. RAN QRH FOR TRAILING EDGE FLAP ASYMMETRY. FLAPS OPERATED APPROX. 5-6 TIMES NO NEEDLE SPLIT NO FAULTS...WRITING A TIZZY FOR FIRST LEG TO MX TO REPLACE THE #
- [SDR SIMA202504143003](https://openairdocs.org/sdr/SIMA202504143003.md): Elec Connector · loose · Apr 13, 2025 · N787BP · Emb ERJ170100LR
  > SLAT FAIL UPON DEPARTURE, UNABLE TO CLEAR USING QRH CHECKLIST. RETURNED TO ORD. INTERRORGATED CMC FOUND FAULT CODE "27811014ACE" TROUBLESHOT WITH FIM 27-81-00-810-807-A00. FOUND RH OUTBOARD SKEW SENSOR #4 CONNECTOR PLUG LOOSE, RETORQUED AND SAFETY WIRED IAE A
- [SDR DALA2025040402553](https://openairdocs.org/sdr/DALA2025040402553.md): Elec Connector · corroded · Apr 1, 2025 · N341NB · Airbus A319114
  > SHIP 3141 DISC: CORROSION TRAILING EDGE ELECTRICAL CONNECTOR ON WING TIP BRAKE LOCATED BETWEEN RIB15 TO RIB16 ON RH WING. C/A: REPLACED ELECTRICAL CONNECTOR OF WING TIP BRAKE ON TRAILING EDGE RH WING AS PER A320 FAM AWM 27-51-14, AIRBUS ESPM 20-44-11-0101, PER
- [SDR SWAA2025033119766](https://openairdocs.org/sdr/SWAA2025033119766.md): Connector · loose · Mar 30, 2025 · N263WN · Boeing 7377H4
  > FLAPS FAILED BETWEEN 1 AND 2; EXTENDED FLAPS TO 15 USING ALT FLAP EXTENSION. RNO MX FOUND LEFT POSITION TRANSMITTER CONNECTOR LOOSE BARELY FINGER TIGHT. CLEANED AND CORRECTLY SECURED. SHOULD BE A GOOD FIX.<[01] ACCOMPLISHED FSEU BITE PER FIM 27-51 TASK 801. FO
- [SDR SWAA2025032508744](https://openairdocs.org/sdr/SWAA2025032508744.md): Wire · loose · Mar 24, 2025 · N7715E · Boeing 7377BD
  > LE FLAP TRANSIT LIGHT ILLUMINATED; FLAP 2 AMBER TRANSIT LIGHT REMAINED ILLUMINATED ON OVERHEAD. PERFORMED QRH. LE FLAP 2 RETRACT SENSOR S170<[01] RESECURED RETRACT SENSOR S170 WIRING PER AMM 27-88-11. ACCOMPLISHED FSEU BITE PER FIM 27-51 TASK 801; NO ACTIVE FA
- [SDR AALA202503100250](https://openairdocs.org/sdr/AALA202503100250.md): Ground Wire · loose · Mar 9, 2025 · N955NN · Boeing 737823
  > AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: NUMBER 1 IN TRANSIT KRUEGER LIGHT WOULD NOT EXTINGUISH WITH ASSOCIATED LEADING EDGE FLAPS TRANSIT LIGHT; AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT DFW. PERFORMED TROUBLESHOOTING PER FIM 27-88
- [SDR SIMA20250308001](https://openairdocs.org/sdr/SIMA20250308001.md): Wire Harness · damaged · Mar 8, 2025 · N332JG · Emb ERJ170200LR
  > SLAT FAIL AFTER TAKE OFF DECLARED EMERGENCY. FOUND R/H OUTBOARD SLAT SKEW SENSOR SHORTED. REMOVED AND INSTALLED SERVICEABLE HARNESS, OPERATED SLAT/FLAPS UP AND DOWN SEVERAL TIMES NO FAULTS NOTED IAW AMM 27-83-01. OP CK GOOD
- [SDR SWAA2025031002282](https://openairdocs.org/sdr/SWAA2025031002282.md): Connector · loose · Mar 5, 2025 · N8515X · Boeing 7378H4
  > ON APPROACH; SELECTED FLAPS 5. NOTICED SLIGHT SPLIT FLAPS 15; FLAPS DID NOT MOVE. FOLLOWED QRH. ALTN FLAPS FUNCTION NORMAL TO 15.<[01] C/W FSEU BITE IAW FIM 27-51 TASK 801. NO CURRENT FAULTS. INSPECTED AND SECURED FLAP POSITION XMITTER CONNECTORS IAW AMM 27-58
- [SDR SWAA2025030502296](https://openairdocs.org/sdr/SWAA2025030502296.md): Elec Connector · failed · Mar 5, 2025 · N261WN · Boeing 7377H4
  > LEADING EDGE FLAPS + SLATS AND TRAILING EDGE FLAPS DID NOT EXTEND WHEN FLAPS LEVER PLACED TO FIVE. FLAP ASYMMETRY INDICATED WHEN ALT FLAP SWITCHED DOWN. LEADING EDGE FLAPS+SLATS EXTENDED<[01] R & R LH FLAP POS TRANSMITTER PER AMM 27-58-01(E148386) <BR>R/R CONN
- [SDR DALA2025030201588](https://openairdocs.org/sdr/DALA2025030201588.md): Connector · damaged · Feb 25, 2025 · N3745B · Boeing 737832
  > (LOG 6594678) L/E FLAP TRANSIT LIGHT INDICATION DURING ELEVATOR CHECKOUT WHEN FLT CNTRL AB SWITCHED TO STDBY RUD POSITION - A/C PITCHED DOWN. REMOVED AND REPLACED LE CRUISE DEPRESSURIZATION VLV IAW B737 AMM 27-81-52. RESEATED RECESSED PIN ON CONNECTOR D1010 IA
- [SDR 21GA20250214001](https://openairdocs.org/sdr/21GA20250214001.md): Circuit Breaker · tripped · Feb 14, 2025 · N652GT · Boeing 767231
  > ON APPROACH GOT TE FLAP FAIL MESSAGE. CREW DECLARED AN EMERGENCY BUT LANDED WITHOUT INCIDENT. FOUND CD OUT. RESET BREAKER. SYSTEM TESTED GOOD.
- [SDR SIMA20250211001](https://openairdocs.org/sdr/SIMA20250211001.md): Wire Harness · damaged · Feb 11, 2025 · N255NN · Emb ERJ170200LR
  > SLAT FAIL AT 3 ON DEPARTURE DVRT ORD TOWER DECLARED EMERGENCY. RAR LH O/B SLAT 3/4 SKEW SENSOR HARNESS IAW EMB 175 AMM 27-83-07 OPS CHECK PASSED NO FURTHER DEFECTS NOTED AT THIS TIME
- [SDR R61A2025020800084](https://openairdocs.org/sdr/R61A2025020800084.md): Wire Harness · faulted · Feb 8, 2025 · N112HQ · Emb ERJ170200LR
  > SLAT FAIL AT FL230. DECLARED EMERGENCY, LANDED WITHOUT FLIGHT. R&R SF-ACE 1. R&R RHOB SLAT SKEW SENSOR HARNESS.
- [SDR DALA2025012100473](https://openairdocs.org/sdr/DALA2025012100473.md): Elec Connector · corroded · Jan 20, 2025 · N347NB · Airbus A319114
  > SHIP 3147 CORROSION ELECTRICAL CONNECTOR FIN: 7543VC AND 7541VC ON I/B FLAP LH WING. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR FIN: 7543VC AND 7541VC ON I/B FLAP LH WING AS PER AIRBUS ESPM 20-44-10. (0770509)

Next page: https://openairdocs.org/jasc/2797/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 jasc_code = '2797'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/2797/reports

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