# Service difficulty reports: Boeing 727-62C

A list on [Boeing 727-62C](https://openairdocs.org/model/boeing-727-62c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 136 reports

- [SDR UPS02239933](https://openairdocs.org/sdr/UPS02239933.md): Battery Pack · discharged · Nov 25, 2002 · N913UP · Boeing 72762C · Emergency Lighting
  > INSPECTION TYPE:IN BOTH EMERGENCY EXITS WILL NOT ARM. R&R BOTH BATTERY PACKS & INSTALLED NEW BATTERIES OPS CHECK GOOD.
- [SDR UPS02239250](https://openairdocs.org/sdr/UPS02239250.md): Pressure Panel · cracked · Sep 2, 2002 · N913UP · Boeing 72762C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:SEG4 RIGHT WHEEL WELL FWD BULKHEAD, JUST BELOW APU LOAD CONTROL VLV, HAS A 3.5 INCH CRACK TO 4 INCH CRACK CRACKED THROUGH. STOP DRILLED CRACK AS PER B72 7 SRM 51-10-01, ACCOMPLISHED HFEC 51-000-00 FIG 4 NDT INSP CRACK CONTAINMENT CONFIRMED. I
- [SDR UPS02237405](https://openairdocs.org/sdr/UPS02237405.md): Battery · discharged · Jan 2, 2002 · N912UP · Boeing 72762C · Emergency Lighting
  > INSPECTION TYPE:PFLT ON PREDEPARTURE CHECK, EMERGENCY EXIT LIGHT AT COCKPIT DOOR INOP. INSTALLED NEW BATTERIES AT COCKPIT DOOR EMERGENCY EXIT LIGHT ASSY, OPS CHECK NORMAL AS PER MM 33-50-1010.
- [SDR UPS01237341](https://openairdocs.org/sdr/UPS01237341.md): Slide · unsecure · Nov 27, 2001 · N912UP · Boeing 72762C · Escape Slide
  > INSPECTION TYPE:N/A ESCAPE SLIDE CAME OFF WHEN CREW CLOSED DOOR. SLIDE RE-INSTALLED NOTE: SLIDE DID NOT DEPLOY.
- [SDR UPS01237191](https://openairdocs.org/sdr/UPS01237191.md): Slide · unsecure · Oct 26, 2001 · N912UP · Boeing 72762C · Escape Slide
  > INSPECTION TYPE:IN DOOR PARTIALLY OPENED FROM EXTERIOR WITH SLIDE ARMED SLIDE FELL FROM DOOR BUT DID NOT DEPLOY. RESECURED SLIDE ASSY.
- [SDR UPS01237071](https://openairdocs.org/sdr/UPS01237071.md): Access Panel · delaminated · Oct 17, 2001 · N913UP · Boeing 72762C · Nacelle/Pylon, Plate/Skin
  > INSPECTION TYPE:C NR 1 PYLON PANEL LOWER SURFACE ACCESS PANEL 5408 HAS DELAMINATION ON UPPER SURFACE. REPAIRED IAW SRM 51-40-20.
- [SDR UPS01237058](https://openairdocs.org/sdr/UPS01237058.md): Panel · cracked · Oct 5, 2001 · N913UP · Boeing 72762C · Trailing Edge Flap Control System
  > INSPECTION TYPE:C RH WING, WHILE BLENDING PAINT FROM A DENT ON PANEL 65-21655-470 IT W AS NOTED THAT THE UPPER SKIN WAS CRACKED REPAIRED IAW SRM 51-40-20
- [SDR UPS01237051](https://openairdocs.org/sdr/UPS01237051.md): Beam · cracked · Oct 4, 2001 · N913UP · Boeing 72762C · Nose/Tail Landing Gear Attach Section
  > INSPECTION TYPE:C SUSPECT CRACK IN NLG DRAGBRACE ATTACH FITTING SUPPORT BEAM IN RT AFT CORNER. REPLACEMENT OF NLG DRAGBRACE SUPPORT BEAM CARRIED OUT IAW UPS EO B72 7-5310-0943 & BOEING DRAWING 65C15724.
- [SDR UPS01237063](https://openairdocs.org/sdr/UPS01237063.md): Structure · corroded · Oct 2, 2001 · N913UP · Boeing 72762C · Rudder Control System
  > INSPECTION TYPE:C SUSPECT CORROSION ON AFT RUDDER CONTROL QUADRANT. REPAIR CARRIED OUT IAW MM 27-20-71, 27-20-00 & DRW 65-20879.
- [SDR UPS01237046](https://openairdocs.org/sdr/UPS01237046.md): Panel · delaminated · Oct 2, 2001 · N913UP · Boeing 72762C · Nacelle/Pylon, Plate/Skin
  > INSPECTION TYPE:C NR 3 PYLON PANEL NR 5501 HAS DELAMINATION AT O/B FWD CORNER. REPAIRED IAW SRM.
- [SDR UPS01237039](https://openairdocs.org/sdr/UPS01237039.md): Stringer · corroded · Oct 2, 2001 · N913UP · Boeing 72762C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON REMOVAL OF FLOOR PANELS FOR CABLE INSPECTION, CORROSION FOUND ON FLOOR BEAM TOP CAP BS 344 RBL6. CORROSION REMOVED IAW SRM 51-10-06, DAMAGE OUT OF LIMITS, REPAIRED I AW SRM 53-10-08
- [SDR UPS01237070](https://openairdocs.org/sdr/UPS01237070.md): Panel · delaminated · Oct 1, 2001 · N913UP · Boeing 72762C · Nacelle/Pylon, Plate/Skin
  > INSPECTION TYPE:C NR 3 PYLON PANEL 5508 ON LOWER SURFACE HAS DELAMINATION ON LOWER SKIN. REPAIRED IAW SRM 51-40-20.
- [SDR UPS01237069](https://openairdocs.org/sdr/UPS01237069.md): Spoiler Panel · delaminated · Oct 1, 2001 · N913UP · Boeing 72762C · Drag Control System
  > INSPECTION TYPE:C L/H WING DELAM ON #1 SPOILER PANEL PANEL REPLACED
- [SDR UPS01237038](https://openairdocs.org/sdr/UPS01237038.md): Stringer · cracked · Oct 1, 2001 · N913UP · Boeing 72762C · Fuselage Main, Structure
  > INSPECTION TYPE:C WHILE INVESTIGATING WING SCANNING LIGHT SUSPECT CRACK STRINGER 15L F OUND CRACKED AT BS 680. DAMAGE BLENDED OUT IAW SRM 53-10-3
- [SDR UPS01237037](https://openairdocs.org/sdr/UPS01237037.md): Stringer · corroded · Sep 30, 2001 · N913UP · Boeing 72762C · Fuselage Main, Structure
  > INSPECTION TYPE:C EVIDENCE OF CORROSION ON STRINGER NESTING SECTION AT BS 440 STR24L STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03
- [SDR UPS01237055](https://openairdocs.org/sdr/UPS01237055.md): Stringer · corroded · Sep 28, 2001 · N913UP · Boeing 72762C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT CORROSION AT BS 1120 STR 19R AREA PAINT STRIPPED, AREA OF SUSPECT CORROSION DERIVETED, SURFACE CO RROSION AND SEALANT REMOVED BETWEEN BS1110-1130 STR19R, STRINGER 19R CUT AND REMOVED AT BS1115-1135, INTERCOSTAL BETWEEN 1110-1130
- [SDR UPS01236903](https://openairdocs.org/sdr/UPS01236903.md): Bracket · cracked · Sep 17, 2001 · N912UP · Boeing 72762C · Engine Thrust Reverser
  > INSPECTION TYPE:C #3 THRUST REVERSER O/B LATCH FAIRING MID ANF AFT BRACKETS ARE CRACKE D. BRACKETS REPLACED IAW MM 78-30-01
- [SDR UPS01236902](https://openairdocs.org/sdr/UPS01236902.md): Strap · cracked · Sep 17, 2001 · N912UP · Boeing 72762C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C NDI INSP OF MID GALLEY DOOR CUTOUT INDICATES REINFORCING STRAP CRACK AT UPPER FWD CUTOUT. REPAIRED IAW UPS EO B727-5330-2685.
- [SDR UPS01236901](https://openairdocs.org/sdr/UPS01236901.md): Trunnion · corroded · Sep 17, 2001 · N912UP · Boeing 72762C · Nose/Tail Landing Gear Attach Section
  > INSPECTION TYPE:C ON REMOVAL OF NLG TRUNNION CAPS CORROSION WAS FOUND IN ALL FOUR BOLT HOLES FOR CLAMPING OF TRUNNION CAPS. REPAIRED IAW SMRO EO 2001-044-001 UPS 727-53-200032.
- [SDR UPS01236877](https://openairdocs.org/sdr/UPS01236877.md): Trunnion · corroded · Sep 17, 2001 · N912UP · Boeing 72762C · Nose/Tail Landing Gear Attach Section
  > INSPECTION TYPE:C ON REMOVAL OF TRUNNION CAPS ON NLG TRUNNION AREA WHERE BUSHINGS WERE INSTALLED HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 53-40-1, 20-20-02, & SMRO EO 2001-044-001.
- [SDR UPS01236876](https://openairdocs.org/sdr/UPS01236876.md): Drum · corroded · Sep 17, 2001 · N912UP · Boeing 72762C · Landing Gear Retraction/Extension System
  > INSPECTION TYPE:C NLG MANUAL EXTENSION AFT DRUM CORRODED. DRUM ASSY REPLACED IAW OHM 32-34-03.
- [SDR UPS01236904](https://openairdocs.org/sdr/UPS01236904.md): Pressure Panel · cracked · Sep 15, 2001 · N912UP · Boeing 72762C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C NDT INSPECTION FOUND CRACK INDICATION AT BS 880 LBL18-19. STOP DRILLED AND HFEC, CRACK CONTAINED. REPAIRED IAW EO B727-5310-04 60.
- [SDR UPS01236890](https://openairdocs.org/sdr/UPS01236890.md): Support Fitting · cracked · Sep 14, 2001 · N912UP · Boeing 72762C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C SUSPECT CRACKS ON LT AND RT 940 SUPPORT FRAME FITTING AT FLOOR BEAM ATTACH FLANGES. HFEC CARRIED OUT LT NDF RT CRACK CONFIRMED ON FWD I/B UPPER FLANGE. REPAIRED IAW UPS EO B727-5310-2954 A.
- [SDR UPS01236905](https://openairdocs.org/sdr/UPS01236905.md): Spar · corroded · Sep 13, 2001 · N912UP · Boeing 72762C · Wing Spar
  > INSPECTION TYPE:C EVIDENCE OF CORROSION ON CENTER TANK FRONT SPAR UPPER CHORD VERTICAL FLANGE AT BS 740 RBL 25. REPAIRED IAW SRM 51-30-02 RBL 19 TO 31.
- [SDR UPS01236445](https://openairdocs.org/sdr/UPS01236445.md): Bulkhead · cracked · Jul 30, 2001 · N912UP · Boeing 72762C · Fuselage Main, Structure
  > INSPECTION TYPE:N/A RT MLG WHEEL WELL FWD BULKHEAD BELOW APU EXHAUST HAS CRACKS AROUND U PPER INBOARD CANNON PLUG RECEPTICLE STA 870 ****MRR FILED AS OPEN*** AIRCRAFT FERRIED TO GSO REPAIR IN PROGRESS FERRY FLIGHT TO GSO
- [SDR UPS01236432](https://openairdocs.org/sdr/UPS01236432.md): Skin · cracked · Jul 29, 2001 · N912UP · Boeing 72762C · Fuselage Main, Structure
  > INSPECTION TYPE:N/A CRACKS AT RH WHEEL WELL AREA STA 870 ***MRR FILED AS OPEN***
- [SDR UPS01234964](https://openairdocs.org/sdr/UPS01234964.md): Light · failed · Feb 6, 2001 · N912UP · Boeing 72762C · Emergency Lighting
  > INSPECTION TYPE:IN COCKPIT EMERGENCY EXIT LIGHT INOP W/OP CHECKED IN FLIGHT. RELAMPED, OPS CHECKS GOOD.
- [SDR UPS01234653](https://openairdocs.org/sdr/UPS01234653.md): Pressure Panel · cracked · Jan 16, 2001 · N912UP · Boeing 72762C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:PFLT 2 INCH CRACK ALONG RT NLG W/W SIDE WALL FWD OF GEAR TRUNNION AT APPROX STA 228 (MARKED). VERIFIED END OF CRACK WITH HFEC. STOP DRILLED RACK IAW 51-40-02 FIG 1. REPAIRED CRACK AS PER SRM 51-40-02 FIG 1. REF LOG PAGE 589676.
- [SDR UPS00232522](https://openairdocs.org/sdr/UPS00232522.md): Fastener · cracked · Apr 30, 2000 · N913UP · Boeing 72762C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CRACK IN FWD CARGO DOOR CUTOUT FWD FRAME INNER FAIL-SAFE STRAP 2ND FASTENER ABOVE STR 23R LOCATED CRACKED FAIL-SAFE STRAP AT BS 522 STR 18-28R. FABRICATED FAIL-SAFE STRAP PER SRM 51-10-2 AND INSTALLED FASTENERS PER SRM 51-30-2.
- [SDR UPS00232469](https://openairdocs.org/sdr/UPS00232469.md): Channel · corroded · Apr 25, 2000 · N913UP · Boeing 72762C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CORROSION (C53-100-01.00-02) ON CHANNEL FROM BS 873 - BS 899 WL 188, LBL 66.5. REMOVED AND REPLACED CHANNEL PER SRM 51-40-3.
- [SDR UPS00232307](https://openairdocs.org/sdr/UPS00232307.md): Line · burst · Apr 11, 2000 · N912UP · Boeing 72762C · Hydraulic System, Main
  > INSPECTION TYPE:C, PRESSURE LINE IN B SYS HYD SERVICE BAY BURST ON OPERATION. FAILED UNDER P-CLIP AREA. PRESSURE LINE IN B-SYS HYD SERVICE BAY REPLACED IAW MM 20-80-01. LEAK CHECKED OK.
- [SDR UPS00232243](https://openairdocs.org/sdr/UPS00232243.md): Web · cracked · Apr 8, 2000 · N912UP · Boeing 72762C · Elevator Structure
  > INSPECTION TYPE:C, WEB BENEATH STAB ACTUATED ELEV TRIM SENSOR CRACKED AT SYS A & SYS B ELEVATOR HYD LINE SUPPORT POINT (PRESS LINES). WEB REPAIRED IAW SRM 51-40-3.
- [SDR UPS00232258](https://openairdocs.org/sdr/UPS00232258.md): Frame · corroded · Apr 7, 2000 · N912UP · Boeing 72762C · Vertical Stabilizer, Spar/Rib
  > INSPECTION TYPE:C, CORROSION ON VERT STAB ON T-CHORD AFT OF FEEL COMPUTER. REPLACED T-CHORD IAW SRM 51-30-2. REF IPC 55-30-00, FIG 2.
- [SDR UPS00232257](https://openairdocs.org/sdr/UPS00232257.md): Stiffener · corroded · Apr 6, 2000 · N912UP · Boeing 72762C · Aerodynamic Fairings
  > INSPECTION TYPE:C, WING TO BODY FAIRING NR 3334 HAS CORRODED STIFFENER AROUND GROUND FAN DOOR CUTOUT (RT). ALSO, CORROSION ON DOOR CUTOUT CORRODED STIFFENER REPAIRED IAW SRM 51-40-3, FIGURE 1. CORROSION FOUND ON CORNER OF DOOR CUTOUT. CORROSION REMOVED, SK
- [SDR UPS00232245](https://openairdocs.org/sdr/UPS00232245.md): Cargo Track · cracked · Apr 6, 2000 · N912UP · Boeing 72762C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C, SUSPECT CRACK FOUND ON TIE DOWN TRACK AT STA 1080, STR 28 RT ADJACENT TO FRAME CUTOUT. REPAIR CARRIED OUT IAW SRM 53-10-5.
- [SDR UPS00232244](https://openairdocs.org/sdr/UPS00232244.md): Channel · cracked · Apr 6, 2000 · N912UP · Boeing 72762C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CRACK ON FLOOR LONGITUDINAL Z SECTION AT BS 1000 AT STR 30 IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-5 FIG 4.
- [SDR UPS00232242](https://openairdocs.org/sdr/UPS00232242.md): Frame · cracked · Apr 6, 2000 · N912UP · Boeing 72762C · Fuselage Main, Frame
  > INSPECTION TYPE:C, CRACK ON FRAME AT BS 1070 STR 29L IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-4.
- [SDR UPS00232241](https://openairdocs.org/sdr/UPS00232241.md): Frame · cracked · Apr 6, 2000 · N912UP · Boeing 72762C · Fuselage Main, Frame
  > INSPECTION TYPE:C, CRACK ON EDGE OF FRAME AT BS 1000 STR 29L IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-4.
- [SDR UPS00232256](https://openairdocs.org/sdr/UPS00232256.md): Web · cracked · Apr 5, 2000 · N912UP · Boeing 72762C · Nacelle/Pylon, Bulkhead/Firewall
  > INSPECTION TYPE:C, LEFT AND RIGHT WEBS AT BS 1387 OVER THE ENGINE 2 HORIZONTAL FIREWALL ARE CRACKED. LT WEB AND BODY SKIN ATTACH TEE REPLACED IAW DRAWING 65-17555.
- [SDR UPS00232061](https://openairdocs.org/sdr/UPS00232061.md): Battery Pack · discharged · Mar 21, 2000 · N913UP · Boeing 72762C · Emergency Lighting
  > EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FWD ENTRY DOOR EMERGENCY EXIT LIGHT BATTERY PACK, SECURED OPS CHECKED GOOD
- [SDR UPS99231094](https://openairdocs.org/sdr/UPS99231094.md): Support · corroded · Nov 8, 1999 · N912UP · Boeing 72762C · Trailing Edge Flaps
  > INSPECTION TYPE AD V LEFT SUPPORT ASSY I/B FLAP TRACK FWD CORRODED. LEFT I/B FLAP TRACK FWD SUPPORT ASSY REPLACED IAW MM 27-51-31.
- [SDR UPS99228532](https://openairdocs.org/sdr/UPS99228532.md): Light · inop · Jan 26, 1999 · N912UP · Boeing 72762C · Emergency Lighting
  > INSPECTION TYPE-N/A, REPEAT WRITE UP WITH EMERGENCY EXIT SWITCH IN THE ARMED POSITION, THE EMERGENCY EXIT LIGHT IN THE COCKPIT IS ON. EMERGENCY EXIT LIGHT BY FWD ENTRY DOOR IS OFF. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AS PER MM 33-50-01. OPS C
- [SDR UPS98228204](https://openairdocs.org/sdr/UPS98228204.md): Skin · corroded · Nov 9, 1998 · N912UP · Boeing 72762C · Rudder, Plate/Skin
  > INSPECTION TYPE:C SURFACE CORROSION ON LOWER RUDDER SKIN PANEL LEFT SIDE BETWEEN FRONT SPAR AND REAR SPAR BY PCU ATTACH POINT. RUDDER REPLACED IAW MM 27-20-1.
- [SDR UPS98228169](https://openairdocs.org/sdr/UPS98228169.md): Frame · cracked · Nov 4, 1998 · N912UP · Boeing 72762C · Fuselage Main, Frame
  > INSPECTION TYPE-C DURING NDT INSPECTION, CRACK FOUND EMANATING FROM FOURTH FASTENER HOLE ABOVE FLOOR LINE AT BS 825.95 RT. REPAIRED IAW APPENDIX C OF EO B727-5310-5474.
- [SDR UPS98228205](https://openairdocs.org/sdr/UPS98228205.md): Skin · corroded · Nov 3, 1998 · N912UP · Boeing 72762C · Rudder, Plate/Skin
  > INSPECTION TYPE:C CORROSION ON LOWER RUDDER SKIN PANEL RT SIDE FRONT SPAR AREA BY PCU ATTACH POIN. RUDDER REMOVED IAW MM 27-20-11.
- [SDR UPS98228166](https://openairdocs.org/sdr/UPS98228166.md): Frame · corroded · Nov 3, 1998 · N912UP · Boeing 72762C · Aerodynamic Fairings
  > INSPECTION TYPE-C, FUSELAGE SLIDING FAIRING NR 3601 HAS CORRODED FRAME AT LOWER FWD CORNER. REPAIRED IAW SRM 53-10-4 AND TYPICAL WEB REPAIRS IAW SRM 51-40-3.
- [SDR UPS98228161](https://openairdocs.org/sdr/UPS98228161.md): Bulkhead Beam · cracked · Nov 3, 1998 · N912UP · Boeing 72762C · Fuselage Main, Bulkhead
  > INSPECTION TYPE-C, CRACK FOUND ON VERTICAL BEAM AT RIGHT BUTTOCK LINE 26.83 AT BS 1183 BULKHEAD CRACK ON VERTICAL BEAM AT RBL 26.85, BS 1183 BULKHEAD REPAIRED IAW APPENDIX D OF B727-5311-0631.
- [SDR UPS98228162](https://openairdocs.org/sdr/UPS98228162.md): Support · corroded · Nov 2, 1998 · N912UP · Boeing 72762C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION ON ANGLE SUPPORT FOR FRONT NET TIE DOWN BS 780 LBL 60.00. ANGLE SUPPORT REPLACED IAW SRM 51-30-2.
- [SDR UPS98228136](https://openairdocs.org/sdr/UPS98228136.md): Intercostal · damaged · Nov 2, 1998 · N912UP · Boeing 72762C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, INTERCOSTAL DAMAGED BS 760 LBL 45 LBL 62. REPAIR CARRIED OUT IAW SRM 51-20-1.
- [SDR UPS98228131](https://openairdocs.org/sdr/UPS98228131.md): Bulkhead · damaged · Nov 2, 1998 · N912UP · Boeing 72762C · Fuselage Main, Bulkhead
  > INSPECTION TYPE-C, FWD PRESSURE BULKHEAD AND STIFFENERS FOUND DAMAGED BS 178 WL 200 RBL 5. REPAIRED IAW UPS EO B727-5310-4290 USING REPAIR KIT 65C36289-1.

Next page: https://openairdocs.org/model/boeing-727-62c/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 = '72762C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-62c/reports

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