# Service difficulty reports: Boeing 757-23A

A list on [Boeing 757-23A](https://openairdocs.org/model/boeing-757-23a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 28 · 1,396 reports

- [SDR FDEA202608261232](https://openairdocs.org/sdr/FDEA202608261232.md): Frame · cracked · Aug 26, 2026 · N919FD · Boeing 75723A · Fuselage Main, Frame
  > RIGHT, BS 1640 FUSELAGE FRAME WEB AT STRINGER 14R UPPER INBD CRACK INDICATION AT 2:00 O'CLOCK, AROUND THE BOTTOM INBD HOLE WITH TWO CRACK INDICATIONS AT 2:00 O'CLOCK AND 7:00 O'CLOCK FACING AFT. FRAME REPAIRED IAW EA F-5310-T0388261, PART 1, & 2. THIS EA DEV
- [SDR FDEA202608251224](https://openairdocs.org/sdr/FDEA202608251224.md): Skin Panel · cracked · Aug 25, 2026 · N919FD · Boeing 75723A · Wing, Plate/Skin
  > LH WING NR 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE SKIN WITH CRACKED. COVE PANEL WITH CRACK AT LH WING # 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE WAS REMOVED, FABRICATED AND INSTALLED IAW B757 SRM 51-40-02-0G AND B-DWG 114N4077 REV D
- [SDR FDEA202608211211](https://openairdocs.org/sdr/FDEA202608211211.md): Power Supply · faulted · Aug 21, 2026 · N917FD · Boeing 75723A · Emergency Lighting
  > R1 EMERGENCY EXIT LIGHT FAILS OPS TEST. PREMATURE REMOVAL/INSTALLATION OFF MPN: 2012-1. REPLACED BATTERY, NO HELP. REMOVED AND REPLACED POWER SUPPLY/TRAY ASSY AND INSTALLED NEW BATTERY, OPS CHECKS NORMAL. OK TO CONTINUE. CHARGER/TRAY REMOVED P/N 201
- [SDR FDEA202608201198](https://openairdocs.org/sdr/FDEA202608201198.md): Battery Pack · failed · Aug 20, 2026 · N939FD · Boeing 75723A · Emergency Lighting
  > INTERIOR EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED FWD BATTERY POWER SUPPLY IAW ABOVE REF. AFTER REPLACMENT FOUND CTR EXIT LIGHT AND R1 EXIT LIGHT OPS CHK SERVICEABLE. L1 DOOR OVERHEAD EXIT LIGHT AND FLT DECK EMER LIGHT INOP. PRESSED COURIER TEST BUT
- [SDR FDEA202608131118](https://openairdocs.org/sdr/FDEA202608131118.md): Floorbeam · corroded · Aug 13, 2026 · N919FD · Boeing 75723A · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM AT BS 1200 BETWEEN BL 0 TO LBL 24.75 WITH CORROSION FLOORBEAM SECTION OUT OF LIMITS AT MAIN CABIN B.S 1200 BETWEEN LBL 5 TO LBL 11 WAS REPAIRED IAW B-757 SRM 53-00-51-2R FIG 201 REPAIR 5.
- [SDR FDEA202608121116](https://openairdocs.org/sdr/FDEA202608121116.md): Seat Track · corroded · Aug 12, 2026 · N919FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BEWTEEN BS 1060 TO 1080 RBL 45.50 WITH CORROSION MAIN CABIN SEAT TRACK SUPPORT (UPPER CHORD) BETWEEN STA 1040-1080 WITH CORROSION OUT OF LIMITS IAW B-757 SRM 53-00-52-1A FIG 101 DETAIL VII WAS REMOVED, FABRICATED AND INSTALLED IAW B
- [SDR FDEA202608121115](https://openairdocs.org/sdr/FDEA202608121115.md): Seat Track · corroded · Aug 12, 2026 · N919FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN SEAT TRACK BETWEEN BS 1180 TO BS 1200 LBL 24.75 OUTB FLANGE WITH CORROSION REMOVED CORROSION AT MAIN CABIN SEAT TRACK AT STA 1180 TO 1200 LBL 24.75 IAW B757 SRM 51-10-02-0G FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101 DETAIL VII
- [SDR FDEA202608081101](https://openairdocs.org/sdr/FDEA202608081101.md): Skin · damaged · Aug 8, 2026 · N919FD · Boeing 75723A · Trailing Edge Flaps
  > EVALUATE EXISTING DOUBLER REPAIR ON RH INBOARD MAIN FLAP LOWER SURFACE, NEAR MF STA 147.00 FOR RSC TRACKING PURPOSE ONLY EXISTING REPAIR ON RH INBOARD MAIN FLAP LOWER SURFACE NEAR MF STA 147.00 WAS EVALUATED UNDER FEDEX EA # F-5750-T0388266 A P1 WITH TIT
- [SDR FDEA202608081100](https://openairdocs.org/sdr/FDEA202608081100.md): Skin · damaged · Aug 8, 2026 · N919FD · Boeing 75723A · Elevator, Plate/Skin
  > EVALUATE EXISTING COMPOSITE REPAIR AT LT ELEVATOR UPPER SURFACE T/E, OUTBOARD AREA. REPAIRED AT LH ELEVATOR UPPER SURFACE T/E, OUTBOARD AREA WAS EVALUATED UNDER E.A.#: F-5520-T0388252 P1.
- [SDR FDEA202607100886](https://openairdocs.org/sdr/FDEA202607100886.md): Lanyard · out of position · Jul 10, 2026 · N917FD · Boeing 75723A · Emergency Exits
  > DURING PREFIGHT FOUND R-1 DOOR WILL NOT ARM. DOOR IS LOCKED AND INDICATED. AMM: 25-66-01-4 FOUND R1 PASSENDER DOOR STATIC LINE CAUGHT IN PUSHROD. REROUTED CARBINER STATIC LINE NO DEFECTS NOTED. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA202606240800](https://openairdocs.org/sdr/FDEA202606240800.md): Unknown · odor · Jun 24, 2026 · N939FD · Boeing 75723A · Air Distribution System
  > AFTER LOWERING MLG THERE WAS A DISTINCT ELECTRICAL BURNING ODOR. EXPERIENCED THIS ABOUT 2 WEEKS AGO ON THIS SAME ACFT. AMM 32-61-00-5 PINNED GEAR & CYCLED GEAR HANDLE WITH HYD APPLIED. ALL INDICATIONS NORMAL IAW AMM, NO ODOR OF OZONE PRESENT. INSPECTED BEH
- [SDR FDEA202605280647](https://openairdocs.org/sdr/FDEA202605280647.md): Adc · faulted · May 28, 2026 · N920FD · Boeing 75723A · Air Data Computer
  > ALTITUDE DISAGREE TWO TIMES DURING DESCENT. FO ALTIMETER MATCHED THE STANDBY AND WAS 400 FEET DIFFERENT THAN CAPTAINS AMM: 34-12-01-4 REMOVED AND REPLACED CAPTAINS ADC. GROUND TEST NORMAL. PARTS INPUT WRI 34-16/ 7188. AMM: 34-12-01-4 REMOVED AND R
- [SDR FDEA202605080570](https://openairdocs.org/sdr/FDEA202605080570.md): Skin · damaged · May 8, 2026 · N939FD · Boeing 75723A · Ailerons
  > LH OUTBOARD AILERON TRAILING EDGE HAS DAMAGE, MARKED WITH TAPE. REPAIRED DAMAGE ON L/H O/B AILERON AT WS 796.26 IN REF TO B757 SRM 57-60-01-2R FIG 201 SH 2 AND B757 SRM 51-70-05-0G FIG 5. CALCULATED NEW BALANCE MOMENT FOR L/H O/B AILERON TO BE -12.30 POUND
- [SDR FDEA202604180469](https://openairdocs.org/sdr/FDEA202604180469.md): Fseu · failed · Apr 18, 2026 · N939FD · Boeing 75723A · Trailing Edge Flap Control System
  > WHILE CONFIGURING FOR LANDING, AS WE SELECTED FLAPS 25, WE RECEIVED A TE FLAPS DISAGREE ON EICAS. INDICATOR REMAINED AT FLAPS 20. COMPLIED WITH QRH. RETRACTED FLAPS USING ALTERNATE METHOD. UNEVENTFUL LANDING IN HNL. EMERGENCY DECLARED. RAN FLAPS THROUGH F
- [SDR FDEA202604030397](https://openairdocs.org/sdr/FDEA202604030397.md): Skin · dented · Apr 3, 2026 · N917FD · Boeing 75723A · Trailing Edge Flaps
  > R/WING O/B T/E MAIN FLAP LOWER SURFACE HAS A DENT PANEL ASSY SKIN OUTER PLY THIS ITEM HAS BEEN ACCOMPLISHED ON EA F-5750-T0386919.
- [SDR FDEA202604020393](https://openairdocs.org/sdr/FDEA202604020393.md): Frame · cracked · Apr 2, 2026 · N917FD · Boeing 75723A · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT WC EF 530-E0329085 D P6 MAIN FRAME BODY STATION 1640 FUSELAGE FRAME INSPECTION FOUND MISSING INTERNAL STRAP IN FRAME AT BS 640 BETWEEN STR 13R TO STR 17R THIS ITEM HAS BEEN ACCOMPLISHED ON FEDEX EA # F-5310-T0353582 TITLE: "FUSELAGE-
- [SDR FDEA202603220365](https://openairdocs.org/sdr/FDEA202603220365.md): Skin · corroded · Mar 22, 2026 · N919FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > #2 ENG. L/H FUSELAGE EXTERIOR COMPOSITE PANEL HAS CORROSION ON OUTER ALUMINUM SKIN AT FWD LWR CORNER NEAR APU PLENUM DRAIN. APPROX. STA. 1904 REF. BOEING DWG. 148N3710. "#2 ENG" LOCATION IS INCORRECT, SEE REMAINDER OF DISCREPANCY REPAIRED L/H FUSELAGE EXTE
- [SDR FDEA202603190358](https://openairdocs.org/sdr/FDEA202603190358.md): Fseu · failed · Mar 19, 2026 · N939FD · Boeing 75723A · Trailing Edge Flap Control System
  > UPON SELECTING FLAPS 25 RECEIVED A TE FLAP DISAGREE EICAS. FLAP HANDLE WAS AT 25 BUT THE FLAPS WERE AT 20. RAN QRH, RETRACTED FLAPS TO UP USING ALT FLAPS AND DIVERTED TO HNL. UNEVENTFUL FLAPS 20 LANDING USING ALT FLAPS. EMERGENCY DECLARED. INTERROGAT
- [SDR FDEA202508291579](https://openairdocs.org/sdr/FDEA202508291579.md): Frame · cracked · Aug 29, 2025 · N918FD · Boeing 75723A · Fuselage Main, Frame
  > CRACK INDICATIONS FOUND IN STA 1640 AT S-14R BOTTOM I/B OPEN HOLE APROX AT 8 O' CLOCK LOOKING AFT AND TWO CRACK INDICATIONS IN UPPER O/B OPEN HOLE APROX AT 6 & 7 O' CLOCK LOOKING AFT COMPLIED WITH EA # F-5310-T0384596 P1 TITLE: FUSELAGE -MAINFRAME -STA 16
- [SDR FDEA202508281562](https://openairdocs.org/sdr/FDEA202508281562.md): Skin · delaminated · Aug 28, 2025 · N918FD · Boeing 75723A · Wing, Plate/Skin
  > LH WING LEADING EDGE SKIN AREA CRACKED BETWEEN WS 150.5 AND 204.50 (#5 LEADING EDGE SLAT AREA) PERFORMED TAP TEST ON LH WING L/E DELAMINATION FOUND DIM L= 18.5" W=15" OUT OF LIMIT IAW B757 SRM 57-41-01-1A FIG 101 SHEET 2 TABLE I NOTE A AND IAW B757 SRM 5
- [SDR FDEA202507301342](https://openairdocs.org/sdr/FDEA202507301342.md): Skin · dented · Jul 30, 2025 · N968FD · Boeing 75723A · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STAB. UPPER SKIN WITH DENT BETWEEN STAB STA 104.248 AND STA 152.248 AND BETWEEN FRONT. SPAR AND AUX SPAR. EVALUATED DENT ON RH HORIZONTAL STAB UPPER SKIN BETWEEN STAB STA 104.248 - 152.248 AND BETWEEN FRONT SPAR & AUX SPAR FOUND THE FOLLW
- [SDR FDEA202507221293](https://openairdocs.org/sdr/FDEA202507221293.md): Socket · loose · Jul 22, 2025 · N921FD · Boeing 75723A · Indicating/Recording System
  > PARKING BRAKE DISCRETE LIGHT DOES NOT ILLUMINATE WHEN PARKING BRAKE SET FOUND PARKING BRAKE LIGHT BASE ASSY LOOSE, TIGHTEN BASE. LIGHT OPS CKED GOOD. A/C OK FOR SERVICE.
- [SDR FDEA202507191267](https://openairdocs.org/sdr/FDEA202507191267.md): Skin · damaged · Jul 19, 2025 · N921FD · Boeing 75723A · Cargo/Baggage Doors
  > WHILE PERFORMING INSPECTION ON THE #2 CARGO DOOR LWR CORNERS SKIN CUTOUT FWD AND AFT, FOUND A REPAIR ON THE AFT LOWER CORNER OF THE #2 CARGO DOOR AREA. AD2006-11-11 FUSELAGE PREVIOUS REPAIR AT NO. 2 CARGO DOOR CUTOUT BS 1410-1445 STR 25- 28R. ACCOMPLISHED S
- [SDR FDEA202507141192](https://openairdocs.org/sdr/FDEA202507141192.md): Floorbeam · corroded · Jul 14, 2025 · N921FD · Boeing 75723A · Fuselage Main, Floor Beam
  > MCD STA 1640 SUPPORT BEAM BL 0.00 TO LBL 45.50 HAS CORROSION. REMOVED CORROSION AT STA 1640 SUPPORT BEAM BL 0.00 - LBL 45050 IAW SRM 51-10-02. FOUND OUT OF LIMIT IAW SRM 53-00-51-1A. REPAIRED FLOOR BEAM AT STA 1640, LBL 45.50 IAW SRM 53- 00-51-2R. MAJOR REP
- [SDR FDEA202507141191](https://openairdocs.org/sdr/FDEA202507141191.md): Crease Beam · corroded · Jul 14, 2025 · N921FD · Boeing 75723A · Fuselage Main, Structure
  > CORROSION NOTED ON THE ATTACHMENT FRAME OF MAIN DECK FLOORBOARD # 252 MKF (RH MOST O/B) AT STA 1540 - 1620. REPAIRED FRAME ATTACHMENT (CREASE BEAM) AT MAIN CABIN R/H STA 1540 - 1620 IAW SRM 53- 00-13-2R. MAJOR REPAIR.
- [SDR FDEA202507111182](https://openairdocs.org/sdr/FDEA202507111182.md): Seat Track · corroded · Jul 11, 2025 · N921FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION NOTED ON THE SEAT TRACK BASE AT LH STA 1200-1240 I/B OF FLOOR PNL 251 MCF. REMOVED AND REPLACED SEAT TRACK AT L/H STA 1180 TO 1240 LBL 45.50 IAW SRM 51-40-02 AND SRM 53-60-52-01. MAJOR REPAIR.
- [SDR FDEA202501270142](https://openairdocs.org/sdr/FDEA202501270142.md): Lens · detached · Jan 27, 2025 · N918FD · Boeing 75723A · Emergency Lighting
  > L EXTERNAL EMERGENCY LIGHT COVER DETACHED. IAW AMM 33-51-06-2-1 EA TF-3350-T0313211 L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK.
- [SDR FDEA202501270140](https://openairdocs.org/sdr/FDEA202501270140.md): Lens · detached · Jan 27, 2025 · N918FD · Boeing 75723A · Emergency Lighting
  > EXTERNAL LH EMER. LIGHT LENSE DETACHED. L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK ADD CLEARED
- [SDR FDEA202501150070](https://openairdocs.org/sdr/FDEA202501150070.md): Battery · failed · Jan 15, 2025 · N920FD · Boeing 75723A · Emergency Lighting
  > EMERGENCY LIGHTS FOR R1 DOOR AND CENTER COURIER AREA INOP. IAW AMM: 33-51-07-2 REMOVED AND REPLACED BATERYPACK ASSY FOR CHARGER ASSEMBLY M730. OPS CHECK GOOD.
- [SDR FDEA202412021762](https://openairdocs.org/sdr/FDEA202412021762.md): Guard · damaged · Dec 2, 2024 · N918FD · Boeing 75723A · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ARE UNARMED WHEN EMERGENCY EXIT LIGHT SWITCH IS CLOSED. FOUND SWITCH GUARD SPRING LOAD OUTSIDE OF THE SWITCH, REPOSITIONED THE SPRING, PERFORMED EMERGENCY LIGHTS OPERATIONAL IAW AMM 33-51-00-5 TEST OK
- [SDR FDEA202409211334](https://openairdocs.org/sdr/FDEA202409211334.md): Skin · dented · Sep 21, 2024 · N919FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > INCOMING A/C DAMAGE JUST BELOW AND FWD OF THE MAIN CARGO DOOR. DENT MEASURING APPROX 2"X3" AND MAX DEPTH OF 0.0119. LOCATED 2" AFT OF FS460 JUST BELOW STR 18L. FUSELAGE - PLATES AND SKINS - INCOMING DENT DAMAGE FWD OF MAIN CARGO DOOR - DOUBLER REPAIR. ACCO
- [SDR FDEA202409111303](https://openairdocs.org/sdr/FDEA202409111303.md): Floorboard · damaged · Sep 11, 2024 · N919FD · Boeing 75723A · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT FLOORBOARD PANEL 252 MWF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MWF ON VTMAE TRAVELER T24/1774253 IAW DRAWING SRZ-25-005 REVISION R MAJOR REPAIR.
- [SDR FDEA202409111302](https://openairdocs.org/sdr/FDEA202409111302.md): Floorboard · damaged · Sep 11, 2024 · N919FD · Boeing 75723A · Fuselage Floor Panel
  > MAIN DECK CARGO COMPT FLOORBOARD PANEL 251 MWF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MWF ON VTMAE TRAVELER T24/1774230 IAW DRAWING SRZ-25-005 REVISION R MAJOR REPAIR.
- [SDR FDEA202409111301](https://openairdocs.org/sdr/FDEA202409111301.md): Floorboard · damaged · Sep 11, 2024 · N919FD · Boeing 75723A · Fuselage Floor Panel
  > MAIN DECK FLOORGOARD PANEL 251MXF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MXF ON VTMAE TRAVELER #T24/1774251 IAW SRZ-25-005 REVISION R DRAWING MAJOR REPAIR.
- [SDR FDEA202408081109](https://openairdocs.org/sdr/FDEA202408081109.md): Skin · corroded · Aug 8, 2024 · N918FD · Boeing 75723A · Fuselage Main, Plate/Skin
  > FOUND EXFOLIATION CORROSION ON EXTERIOR SKIN SURFACE ADJACENT TO L/H APY DOOR FWD HINGE POINT AREA COMPLIED WITH MAJOR REPAIR CLASSIFICATION. E.A. #-F-5330-T0380244 P1 FUSELAGE-PLATES AND SKIN- LH APU COMPARTMENT SKIN PANEL REPAIR BETWEEN STA. 1885.20 AND
- [SDR FDEA202407251057](https://openairdocs.org/sdr/FDEA202407251057.md): Relay · failed · Jul 25, 2024 · N918FD · Boeing 75723A · Landing Gear Steering System
  > NOSE L/G COMPONENTS INSPECTION REQUIRED TO CONFIRM NO DAMAGES. NOSE GEAR COMPONENTS VISUAL INSPECTION PERFORMED. NO OBVIOUS DAMAGES OBSERVED. ALSO NOSE GEAR STEERING OPERATIONAL TEST PERFORMED SATIS REF AMM 32-51-00-5-3.
- [SDR FDEA202407251056](https://openairdocs.org/sdr/FDEA202407251056.md): Relay · failed · Jul 25, 2024 · N918FD · Boeing 75723A · Fuel Controlling System
  > RUNWAY ENGINE START. INSTEAD OF STABILIZING AT IDLE, THE RPM AND THRUST INCREASED WITH NO THROTTLE INPUT AND THROTTLES AT IDLE AND CONTINUED TO INCREASE RAPIDLY UNTIL CREW CUTOFF FUEL. SLIGHTLY PUSHED THE TUG. EVERYONE IS OK. APPLIED AND IDLE CONTROL RELA
- [SDR FDEA202407211036](https://openairdocs.org/sdr/FDEA202407211036.md): Battery Pack · no test · Jul 21, 2024 · N922FD · Boeing 75723A · Emergency Lighting
  > ON SERVICE CHECK FOUND EMERGENCY EXIT AISLE SIGN NOT ILLUMINATING WHEN EMERGENCY LIGHTS TEST PERFORMED. AMM: 33-51-07-2-0, REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK AS PER 757 AMM 33-51-07-2-0. OPS CHECK GOOD. AIRCRAFT OK FOR SER
- [SDR FDEA202406230855](https://openairdocs.org/sdr/FDEA202406230855.md): Battery Pack · failed · Jun 23, 2024 · N917FD · Boeing 75723A · Emergency Lighting
  > DURING SVC FOUND THE L1 INSIDE AND OUT EMERGENCY LIGHTS WERE INOP. REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK AS REQUIRED IAW AMM 33-51-07-2. OPS CHECK GOOD.
- [SDR FDEA202406010758](https://openairdocs.org/sdr/FDEA202406010758.md): Support · damaged · Jun 1, 2024 · N919FD · Boeing 75723A · Trailing Edge Flaps
  > L/H WING, AFT FAIRING SUPPORT INBD MAIN FLAP FITTING IS LOOSE. FOUND AFT MOUNT HOLE DAMAGED IN LH I/B LWR MAIN FLAP FOR FAIRING SUPPORT BRACKET. REPAIRED DAMAGED HOLE AND REPLACED BRACKET REF. B757 SRM 57-53-02-2R REPAIR 3. AND INSTALLED FAIRING TO BRACKET R
- [SDR FDEA202405250726](https://openairdocs.org/sdr/FDEA202405250726.md): Controller · failed · May 25, 2024 · N921FD · Boeing 75723A · Cabin Pressure Controller
  > AT FL400 CABIN ALT HIGH WARNING DONNED MASKS. RAN QRH. INITIATED EMERGENCY DESCENT. CABIN ALTITUDE RATE REACHED 2000 FT PER MIN DOWN AND HIGHEST ALTITUDE REACHED WAS 15 K. EMERGENCY DECLARED AMM: 21-31-02-4, AMM: 21-31-00-5, AMM: 05-51-24-2, CABIN PRE
- [SDR FDEA202404300520](https://openairdocs.org/sdr/FDEA202404300520.md): Fan · failed · Apr 30, 2024 · N918FD · Boeing 75723A · Air Distribution Fan
  > OIL BURNING SMOKE BELOW 5000FEET WITH LOW POWER SETTING. R & R L/H RECIRCULATION FILTER AND FAN, REVERSED MEL 21-25-01-02 & MEL 21-58-07, RECONNECTED WIRE ON PLUG D40910J, PERFORMED LT RECIRCULATION FAN & EQUIPMENT COOLING TEST, ALL TESTS PASSED, LEAK CHEC
- [SDR FDEA202404230272](https://openairdocs.org/sdr/FDEA202404230272.md): Girt Bar · out of alignment · Apr 23, 2024 · N918FD · Boeing 75723A · Emergency Equipment
  > LIGHT ON LEFT CREW ENTRY DOOR INOP. FACT 23APR24 08:51 AMS AMM: 25-66-10-2 AMM: 25-66-11-2 RELAMP NO HELP. FOUND SLIDE VERY HARD TO ARM AND GIRTBAR FITTINGS NOT REACHING THE TARGETS. RE-INSTALLED GIRTBAR FLAP AS PER AMM 25-66-10-2 REV 133.9 VERIFED
- [SDR FDEA202404030435](https://openairdocs.org/sdr/FDEA202404030435.md): Lamp · burned out · Apr 3, 2024 · N939FD · Boeing 75723A · Emergency Lighting
  > L1 MAIN ENTRY DOOR SLIDE LIGHT IS BURNT OUT. REMOVED AND REPLACED BOTH BULBS AND PERFORMED ADJUSTMENT TEST IAW AMM 52-11-00-2-0, TEST SATIS, A/C OK FOR SERVICE.
- [SDR FDEA202404010430](https://openairdocs.org/sdr/FDEA202404010430.md): Skin · corroded · Apr 1, 2024 · N922FD · Boeing 75723A · Wing, Plate/Skin
  > R / WING DRY BAY ACCESS PANEL 644AB WING NUT PLATES DAMAGED WITH POSSIBLE EXFOLIATION ON WING SKIN. COMPLIED WITH EA F-5730-T0378521 P1 WINGS-PLATE AND SKIN CORROSION R/H WING LOWER DRY BAY PANEL REPAIR AT ACCESS PANEL CUTOUT 644 AB, WS 775-806 WITH NO DEV
- [SDR FDEA202403290410](https://openairdocs.org/sdr/FDEA202403290410.md): Web · corroded · Mar 29, 2024 · N922FD · Boeing 75723A · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT F. STA BETWEEN 600-620 RBL 64.5 SHEAR WEB HAS CORROSION AFTER EVALUATED SHEAR WEB AT F.STA 600 TO 620 AND BTW RBL 62.89 - 64.5 FOUND OUT OF LIMITS IAW B-757 SRM 53-30-13-1A FIG 101 DETAIL III; REMOVED, FABRICATED AND INS
- [SDR FDEA202403290408](https://openairdocs.org/sdr/FDEA202403290408.md): Fairing · gouged · Mar 29, 2024 · N922FD · Boeing 75723A · Aerodynamic Fairings
  > SEC 48 F.ST 1862.2 S.14BL HAS TYPICAL GOUGE CAUSED BY STAB BLADE SEAL L/H CLEANED GOUGED AREA ON TWO DIFERENT PARTS AFFECTED ( PANEL FAIRING) IAW B-SOPM 20-30-03 AND AFTER EVALUATION TWO DIFERENT AREAS FOUND # 1 AREA AT STA 1862 TO STA 1865 FOUND WITHI
- [SDR FDEA202403280399](https://openairdocs.org/sdr/FDEA202403280399.md): Seat Track · corroded · Mar 28, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN FOUND CORROSION ON SEAT TRACK STA 1180-1200 RBL45.50 REMOVED CORROSION AT SEAT TRACK FLANGE BETWEEN STA. 1180-1200 RBL 45.50, EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-52-1A FIG. 101 DETAIL VIII REMOVED AND INSTALLED NEW SEAT
- [SDR FDEA202403280391](https://openairdocs.org/sdr/FDEA202403280391.md): Window · cracked · Mar 28, 2024 · N919FD · Boeing 75723A · Flight Compartment Windows
  > WHILE IN CRUISE FLIGHT FL360, CAPTAIN SIDE FRONT WINDSCREEN ARCED FOLLOWED BY SHATTERING WITH OUTER PAIN. RAN QRH, ARCING CONTINUED. POSSIBLE DEFORMED WINDOW WITH CONTINUING ARCING THROUGHOUT DESCENT. EMERGENCY DECLARED. REMOVED & REPLACED L1 WINDOW AS PER
- [SDR FDEA202403270388](https://openairdocs.org/sdr/FDEA202403270388.md): Seat Track · corroded · Mar 27, 2024 · N922FD · Boeing 75723A · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK HAS EVIDENCE OF CORROSION ALONG FLANGE UNDER CRACKED PAINT BETWEEN STA 1320-1420 RBL-44 REMOVED CORROSION AT SEAT TRACK I\B FLANGE BETWEEN STA 1320-1420 RBL44 IAW B757 SRM 51-10-02-0G, EVALUATED AREAS FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00

Next page: https://openairdocs.org/model/boeing-757-23a/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 aircraft_model_key = '75723A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-757-23a/reports

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